Oscar-7, the LAZARUS Satellite article by GM1SXX
This page is a work in progress. I hope to add more information as time permits.

Oscar-7 is a thirty year old amateur radio satellite with an amazing 'secret' ... it still WORKS!
The batteries went short circuit many years ago. This effectively ended the mission of Oscar-7.It came back to life in June 2002 ... but only working when in sunlight, because the short circuited batteries went open circuit thus allowing the bird to work when in sunlight. The satellite cannot be guaranteed to start up in any specific mode, but it DOES still function
In December 2003 John LA2QAA and Al GM1SXX decided to see what sort of shape the satellite was in after being dead for over 20 years. The answer turned out to be a surprise. Conditions on board were pretty good when in sunlight with temperatures, voltages and other telemetry being close to nominal values although as might be expected, the half-battery voltage reading was nonsense.
Despite what is being said in some quarters, the solar panels do provide a reasonable amount of power when in sunlight and when the telemetry system work, it returns some sensible data. Its fairly normal for the C.W. telemetry to have a pronounced warble while the transponder works OK.
From a serious satellite operators point of view, this is a superb satellite. Unlike the FM 'me-too' EZ-sat's, this bird can actually support concurrent QSO's, something you just can't do on an FM bird. Just make sure you optimise you RECEIVE system before trying to use this bird.
A-O-7 in a high near circular polar retrograde orbit and is capable of providing real DX contacts.
Most importantly, DO NOT hit this bird with a lot of uplink power. Unlike FM 'EE-ZEE' sat's (as stupid a name as I've ever heard for an inappropriate technology) it can support multiple QSO's and has a VERY sensitive RX.
5 watts to an 8 ele yagi should be plenty. If it isn't, FIX YOUR RECEIVE SYSTEM.
Keep the uplink power to the absolute minimum, have fun, work DX and enjoy this superb bird while you can.
Despite the obvious need for a replacement LINEAR polar satellite to replace this bird, AMSAT appear to have all but abandoned this class of tremendously useful comsat, instead favouring very expensive and complex Molniya birds, FM 'EE-ZEE sat's (where's the challenge and self-training aspect there?) and University 'me-too' birds that hijack amateur radio frequencies to return what should effectively be commercial data.
I'm certainly not the first person to question the use of amateur radio frequencies for what amounts to commercial projects. Have a look at John Branegan's SATGEN on the very issue. You can find the SATGENS elsewhere on this website.
So, enjoy Oscar-7 while you can. Short of the Russians finding the cast to launch another RS bird (highly unlikely, but I'd LOVE to be proven wrong here), there will never be another bird as versatile as Oscar-7.
Here are the basic data on Oscar-7.
Name: AMSAT-OSCAR 7 (Phase-IIB)
Nasa Catalog Number: 7530
Launched: November 15, 1974
Launch vehicle: Delta 2310
Launched piggyback with: ITOS-G (NOAA 4) and the Spanish INTASAT
Launch location: Vandenberg Air Force Base, Lompoc, California
Weight: 28.6 kg
Orbit: 1444 x 1459 km
Inclination: Inclination 101.7 degrees
Period:
Size: Octahedral shaped 360 mm high and 424 mm in diameter
Modes: A, B, and C
Beacons:
29.502 MHz (200 mw) (Now inoperative... GM1SXX)
145.972 MHz (200 mw) Used in conjunction with Mode B and C [low power Mode B]
435.100 MHz (intermittent problem -- switches between 400 mw and 10 mw)
2304.1 MHz (40 mw) (Now inoperative... GM1SXX)
Transponder I: Mode A
Type: linear, non-inverting
Uplink: 145.850 - 145.950 MHz
Downlink: 29.400 - 29.500 MHz
Translation Equation:
Downlink (MHz) = Uplink (MHz) - 116.450 MHz +/-
Doppler
Output Power: 1.3 watts PEP (start of life)
Transponder II: Mode B and Mode C (low power)
Type: linear, inverting
Uplink: 432.125 - 432.175 MHz *See Note
Downlink: 145.975 - 145.925 MHz
Translation Equation:
Downlink (MHz) = 578.100 - uplink (MHz) +/- Doppler
Output Power: 8 watts PEP Mode B (start of life), 2.5 watts PEP Mode C
*Note: Due to changes in Amateur Service and Amateur Satellite Service there are questions as to legality of Amateurs transmitting to AO-7. The uplink frequency predates the WARC '79 allocation of 435-438 MHz by the ITU for the Amateur Satellite Service and places the uplink in 70cm weak signal segment.
Potential users should realize that when they are uplinking to a satellite, they are no longer operating in the Amateur Service but instead operating in the Amateur Satellite Service. Thus they are subject to Amateur Satellite Service rules. Therefore uplinking to AO-7 is possibly illegal since the Amateur Satellite Service is not permitted at 432.1 MHz. Also, since the IARU bandplan has the 432.1 MHz range earmarked as "weak signal" in all three Regions, it would appear that all users trying to access the uplink are also outside the Amateur Satellite Service rules and regulations.
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Lazarus Returns
The item below is from the AMSAT archives.
Date: Sat, 22 Jun 2002 16:00:08 -0600
To: amsat-bb@AMSAT.Org, bod@AMSAT.Org
From: Jim White <jim@coloradosatellite.com>
Subject: [amsat-bb] AO-7 info from Jan
Folks, Following are two messages from Jan King regarding the signal Pat heard the other night on 145.975. It clearly was OSCAR-7. Jan's messages pretty much speak for themselves. Pretty amazing story. Jim jim@coloradosatellite.com
My God, I can't believe what Pat was hearing. It has to be AMSAT-OSCAR-7 according to the frequency. AO-6 had a 70 cm beacon, which failed fairly quickly after launch, and a 2m up/10m down transponder (the original Mode A transponder). AO-8 had another Mode A transponder and the first Mode J transponder built by the Japanese. That was, of course, backwards from Mode B or 2m up/70 cm down. But, AO-7 had both a Mode A and a MODE B transponder. Mode B had a downlink on 2m. So, of those three satellites, AO-7 is the only one that had a downlink on 2m. Let me go out to the garage and check the frequency. --------- Time Passed Here.--------- Well, the garage files aren't what they once were. Most of the original files were there but, the Karl Meizer - Mode B file is missing! Damn. Also missing are the log books, which are historically valuable. The logs aren't lost. I packed them away with my office stuff somewhere in my garage boxes which second as a warehouse - so I wouldn't lose them. :-( But, I knew I had lots of stuff that would tell the frequency plan. The first thing I found as I was looking was an old ARRL booklet called, "Getting to Know OSCAR from the Ground Up." I seem to have been a co-author. Hmmm. Don't even remember it. The transponder had an uplink at 432.125 MHz to 432.175 MHz. The passband was inverting and a little less than 50 kHz wide. The downlink passband was from 145.925 to 145.975 MHz. THE BEACON WAS AT 145.975 MHz. If I can find the log books I can tell you how far off the nominal frequency the beacon was as measured back in November 1974 just before launch. So Pat was hearing AO-7, 24 years after it died! Whew!! Here's probably what's happening. That thing has a good set of arrays and the first BCR (battery charge regulator) we ever flew. It's the first spacecraft we ever had that was capable of overcharging the battery. When the battery failed the cells began to fail short. One cell after another failed and the voltage measured on telemetry began to drop. So, the cells were clearly failing SHORT. Now, after all these years, what happens if any one of the cells loses the short and becomes open? Then, the entire power bus becomes unclamped from ground and the spacecraft loads begin to again be powered but, this time only from the arrays. Now you have a daytime only satellite but, each time the sun rises at the spacecraft you have a random generator that either turns on Mode A or Mode B or whatever it wants. So, occasionally that 70cm/2m transponder transmitter and beacon must least work. From what you have told me (and without going back and decoding the old telemetry equations) I can tell you that the following things work in that spacecraft: The arrays, the BCR, the ISR (instrumentation switching regulator), the Mode B transmitter and beacon injection circuitry, the Morse Code telemetry encoder, and the voltage reference circuitry. The latter I know is working because the last telemetry value is 651. The "6" is just the row number of the telemetry value but the 51 means that the 1/2 volt reference is measuring 0.51 volts. I know that telemetry equation by heart since it was used as the calibration value for the rest of the telemetry system. So the telemetry has a fair chance of being decoded and making some sense!!! How about that, man? Jim that's all amazing for someone who was as close to that thing as I was. You must remember, that spacecraft was built in my house (in a basement laboratory) in Lanham, Maryland. Werner and Karl were putting the finishing touches on that transponder when Ian, my son was being born in the upstairs bedroom. That afternoon Donna and I went to the hospital to have the baby while Karl and Werner continued final debugging! So, it doesn't get much more personal than that. As the man said, "It's most remarkable." You can post this to the AMSAT-bb if you want. 73's, Jan W3GEY AMSAT-OSCAR-7 Project Manager :-)
Well Jim, G3IOR's telemetry frame is interesting. Apparently he did hear the AO-7 Mode B beacon tonight. I got out my December 1974 and looked up the telemetry equations for the Morse Code Telemetry Encoder and what I found is in the attached spreadsheet. I'm blown away. Most of this stuff makes pretty good sense. In particular, the temperatures make sense and I would have guessed that they would be the most sold IF the reference voltage held (which it did). Interpreting some of this for those who may not understand or don't remember, the telemetry says the spacecraft was in Mode B; all the other beacons and Mode A were off. It is possible that the thing had just turned on because the old 24 hour timer just reset it to Mode B. The damn thing may think it is still on an every other day cycle. The power output of the transponder is 1.16 watts which may mean it is transmitting white noise plus beacon power. That seems about right, but a little low as I recall. The instrumentation switching regulator is in the middle of it's normal range and seems to be working fine. The internal temperatures are around 15 deg. C; the external temperatures are around 5 C and the transponder PA temp, which should be the warmest - IS - it's 35.1 deg. C. The array current value is bust. I think maybe it always was. Need to look for some old telemetry to confirm that. The array current calibrations looks off. The array currents are in the normal range but all four show current. This can't be. Only two at a time should show current. Without a battery on line, this is entirely possible. The big find is that the battery voltage telemetry shows a voltage of 13.9 volts. Normal is 13.6 to 15.1 volts. So that would suggest the battery was normal BUT, the 1/2 battery voltage is measuring only 5.8 volts. That can't be. This imbalance probably means that the 5.8 volts is the correct value for the lower half of the battery (which is a low value for that half, if the cells were normal - they are probably not) and there is a break somewhere in the upper 1/2 of the battery string. My guess is the indicated voltage is really what the BCR is putting out with only the spacecraft load as a real load and the battery string has an effective break (or a pretty high resistance) somewhere in the upper half. So, this old war horse of a spacecraft seems to have come back from the dead if only for a few moments. And it is telling us, that even in a 1460 km high orbit a cheap spacecraft built by a bunch of hams, without very many high rel parts and without designing for a radiation dose like this, can last for 27+ years in space as far as a majority of it's electronics is concerned. Even the damn precision reference voltage regulator is still in calibration! Pitty Pat did not recognize his old friend when he saw him again. Well Jim, you made my day!
73's, Jan
A-O-7 Telemetry
The satellite transmits telemetry on its beacon downlink as a series of morse code digits
The data are transmitted in the following format...
AO-7 telemetry format:
1aa 1bb 1cc 1dd 2aa 2bb 2cc 2dd 3aa 3bb 3cc 3dd 4aa 4bb 4cc 4dd 5aa 5bb 5cc 5dd 6aa 6bb 6cc 6dd Hi Hi
This data requires that appropriate equations are applied to produce meaningful results
You should note that good data frames always end in 649,650 or 651. Other values should be regarded as not trustworthy.
Oscar-7 used a single A/D converter with a voltage reference source. The reference voltage of the source is the last value of the last item in the frame (channel 6dd Midrange Telemetry Calibration) and the raw uncalculated value as CW from the bird should be 649, 650 or 651.
AMSAT-OSCAR-7 Telemetry Information
| Channel Measured Parameter | Measurement Range | Calibration Equation (Preliminary) |
| 1A Total Solar Array Current | 0 to 3000 ma | I = 29.5 N (ma) |
| 1B +X Solar Panel Current | 0 to 2000 ma | I = 1970 - 20N (ma) |
| 1C -X Solar Panel Current | 0 to 2000 ma | I = 1970 - 20N (ma) |
| 1D +Y Solar Panel Current | 0 to 2000 ma | I = 1970 - 20N (ma) |
| 2A -Y Solar Panel Current | 0 to 2000 ma | I = 1970 - 20N (ma) |
| 2B RF Power Out 70cm/2m | 0 to 8 watts | P = 8(1 - 0.01N)^2 (watts) |
| 2C 24 Hour Clock Time | 0 to 1440 min. | t = 15.16N (min) |
| 2D Battery Charge/Discharge | -2000 to 2000 ma | I = 40(N - 50) (ma) |
| 3A Battery Voltage | 6.4 to 16.4 V | V = 0.1N + 6.4 (volts) |
| 3B Half-Battery Voltage | 0 to 10 V | V = 0.10N (volts) |
| 3C Bat. Chg. Reg. #1 | 0 to 15 V | V = 0.15N (volts) |
| 3D Battery Temperature | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 4A Baseplate Temperature | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 4B PA Temp. 2m/10m | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 4C +X Facet Temp. | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 4D +Z Facet Temp. | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 5A PA Temp. 70cm/2m | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 5B PA Emit. Current 2m/10m | 0 to 1167 ma | I = 11.67N (ma) |
| 5C Module Temp. 70cm/2m | -30 to +50 deg. C | T = 95.8 - 1.48N (deg. C) |
| 5D Instrument Sw. Regulator Input Current | 0 to 93 ma | I = 11 + 0.82N (ma) |
| 6A RF Power Out 2m/10m | 0 to 10,000 mw | P = (N^2)/1.56 (mw) |
| 6B RF Power Out 70 cm | 0 to 1,000 mw | P = 0.1(N^2) + 35 (mw) |
| 6C RF Power Out 13 cm | 0 to 100 mw | P = 0.041(N^2) (mw) |
| 6D Midrange Telemetry Calibration | 0.500 V | V = 0.01N(0.50 +/- 0.01) (V) |