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
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 1292U 65016C 26046.89998191 .00000161 00000-0 14143-3 0 9998
2 1292 70.0754 212.3950 0017103 114.0516 246.2385 14.01544679107572Epoch: 2026-02-15T21:35Z
TLE epoch observation values (Epoch: 2026-02-15T21:35:58.437Z)
Latitude
0°
Longitude
102.49946°
Altitude
895.801 km
Speed
7.402 km/s
True Right ascension
14h 09m 34s
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
16:11:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
898.906 km
Perigee altitude
874.057 km
Semi-major axis
7,264.618 km
Eccentricity
0.00171
Inclination
70.0754°
RAAN
212.395°
Arg. of periapsis
114.0516°
True anomaly
246.05928°
Mean anomaly
246.2385°
Eccentric anomaly
246.14888°
Mean motion
3.50529 °/min
Orbital period
102.7 mins
BSTAR
0.00014143
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-16 20:24:25.217Z | 7.578° NNE | 2026-02-16 20:28:25.217Z | 52.375° ENE | 17.417° | 2026-02-16 20:31:25.217Z | 86.449° E |
| 10 mins | 2026-02-16 22:09:25.217Z | 330.832° NNW | 2026-02-16 22:14:25.217Z | 210.11° SW | 43.362° | 2026-02-16 22:19:25.217Z | 164.609° S |
| 9 mins | 2026-02-17 11:24:25.217Z | 162.778° S | 2026-02-17 11:28:25.217Z | 102.75° ESE | 30.589° | 2026-02-17 11:33:25.217Z | 41.82° NE |
| 9 mins | 2026-02-17 13:09:25.217Z | 246.497° WSW | 2026-02-17 13:13:25.217Z | 302.67° NW | 28.908° | 2026-02-17 13:18:25.217Z | 6.024° 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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