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, 15.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GGSE 3
1 01292U 65016C 26208.18965724 .00000085 00000-0 90821-4 0 9999
2 01292 70.0747 225.6585 0022109 258.0929 101.7701 14.01597925130175Epoch: 2026-07-27T04:33Z
TLE epoch observation values (Epoch: 2026-07-27T04:33:06.385Z)
Latitude
-0.00004°
Longitude
-147.49492°
Altitude
893.902 km
Speed
7.404 km/s
True Right ascension
15h 02m 38s
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
22:42:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.358 km
Perigee altitude
870.236 km
Semi-major axis
7,264.434 km
Eccentricity
0.00221
Inclination
70.0747°
RAAN
225.6585°
Arg. of periapsis
258.0929°
True anomaly
102.01798°
Mean anomaly
101.7701°
Eccentric anomaly
101.89406°
Mean motion
3.50542 °/min
Orbital period
102.7 mins
BSTAR
0.000090821
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-28 10:13:24.653Z | 22.654° NE | 2026-07-28 10:15:24.653Z | 43.173° NE | 12.3° | 2026-07-28 10:17:24.653Z | 63.821° ENE |
| 10 mins | 2026-07-28 11:57:24.653Z | 342.783° N | 2026-07-28 12:01:24.653Z | 38.296° NE | 42.845° | 2026-07-28 12:07:24.653Z | 147.652° SSE |
| 5 mins | 2026-07-28 13:44:24.653Z | 282.301° WNW | 2026-07-28 13:46:24.653Z | 259.078° W | 15.705° | 2026-07-28 13:49:24.653Z | 226.924° WSW |
| 7 mins | 2026-07-29 01:13:24.653Z | 136.429° SSE | 2026-07-29 01:16:24.653Z | 97.043° ESE | 20.98° | 2026-07-29 01:20:24.653Z | 53.516° ENE |
| 10 mins | 2026-07-29 02:56:24.653Z | 226.664° WSW | 2026-07-29 03:00:24.653Z | 282.711° WNW | 38.092° | 2026-07-29 03:06:24.653Z | 14.813° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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