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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Edit Public Description
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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GGSE 3
1 01292U 65016C 26034.98139506 .00000106 00000-0 10502-3 0 9996
2 01292 70.0747 238.0176 0017517 131.9245 228.3361 14.01539008105905Epoch: 2026-02-03T23:33Z
TLE epoch observation values (Epoch: 2026-02-03T23:33:12.533Z)
Latitude
-0.00001°
Longitude
110.56085°
Altitude
899.269 km
Speed
7.398 km/s
True Right ascension
15h 52m 04s
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
17:33:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
899.226 km
Perigee altitude
873.776 km
Semi-major axis
7,264.638 km
Eccentricity
0.00175
Inclination
70.0747°
RAAN
238.0176°
Arg. of periapsis
131.9245°
True anomaly
228.18636°
Mean anomaly
228.3361°
Eccentric anomaly
228.26121°
Mean motion
3.50528 °/min
Orbital period
102.7 mins
BSTAR
0.00010502
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Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
Did you know?
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 | 2026-02-04 16:55:18.046Z | 298.197° NW | 2026-02-04 16:57:18.046Z | 319.522° NNW | 12.442° | 2026-02-04 16:59:18.046Z | 340.032° N |
| 9 mins | 2026-02-05 00:06:18.046Z | 346.326° N | 2026-02-05 00:10:18.046Z | 51.951° ENE | 41.1° | 2026-02-05 00:15:18.046Z | 141.071° SSE |
| 5 mins | 2026-02-05 01:53:18.046Z | 282.464° WNW | 2026-02-05 01:55:18.046Z | 257.232° W | 17.542° | 2026-02-05 01:58:18.046Z | 223.099° SW |
| 6 mins | 2026-02-05 13:22:18.046Z | 134.591° SE | 2026-02-05 13:25:18.046Z | 98.443° ESE | 18.449° | 2026-02-05 13:28:18.046Z | 63.777° ENE |
| 10 mins | 2026-02-05 15:05:18.046Z | 221.372° SW | 2026-02-05 15:09:18.046Z | 275.444° WNW | 40.081° | 2026-02-05 15:15:18.046Z | 16.762° 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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