GGSE 3, 1292
Orbit data source: Space-Track
GGSE 3, 1292 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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1292 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL 24", Unknown motor
Mass
59 kg wet, 59 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
SPHERE + 3 ANT, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GGSE 3
1 01292U 65016C 26271.20546218 .00000041 00000-0 62292-4 0 9998
2 01292 70.0749 90.1816 0019101 180.1523 179.9584 14.01613048139004Epoch: 2026-09-28T04:55Z
TLE epoch observation values (Epoch: 2026-09-28T04:55:51.932Z)
Latitude
0.00001°
Longitude
9.22706°
Altitude
904.42 km
Speed
7.393 km/s
True Right ascension
06h 00m 43s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:38:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.121 km
Perigee altitude
872.369 km
Semi-major axis
7,264.382 km
Eccentricity
0.00191
Inclination
70.0749°
RAAN
90.1816°
Arg. of periapsis
180.1523°
True anomaly
179.95856°
Mean anomaly
179.9584°
Eccentric anomaly
179.95848°
Mean motion
3.50546 °/min
Orbital period
102.7 mins
BSTAR
0.000062292
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Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GGSE 3 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-09-28 22:36:29.975Z | 345.875° N | 2026-09-28 22:41:29.975Z | 47.084° ENE | 50.616° | 2026-09-28 22:47:29.975Z | 137.034° SSE |
| 7 mins | 2026-09-29 00:23:29.975Z | 297.696° NW | 2026-09-29 00:26:29.975Z | 260.359° W | 22.422° | 2026-09-29 00:30:29.975Z | 212.703° SW |
| 5 mins | 2026-09-29 11:54:29.975Z | 122.324° SE | 2026-09-29 11:56:29.975Z | 99.455° ESE | 16.401° | 2026-09-29 11:59:29.975Z | 66.963° ENE |
| 10 mins | 2026-09-29 13:36:29.975Z | 214.161° SW | 2026-09-29 13:41:29.975Z | 329.079° NNW | 67.014° | 2026-09-29 13:46:29.975Z | 19.496° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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