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: 11 hours ago
TLE from 11 hours ago
0 GGSE 3
1 1292U 65016C 26137.10876819 .00000070 00000-0 81384-4 0 9996
2 1292 70.0785 18.4727 0019970 343.4658 16.5797 14.01577573120212Epoch: 2026-05-17T02:36Z
TLE epoch observation values (Epoch: 2026-05-17T02:36:37.571Z)
Latitude
-0.00006°
Longitude
104.50002°
Altitude
876.754 km
Speed
7.421 km/s
True Right ascension
01h 13m 53s
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
21:55:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.875 km
Perigee altitude
871.86 km
Semi-major axis
7,264.504 km
Eccentricity
0.002
Inclination
70.0785°
RAAN
18.4727°
Arg. of periapsis
343.4658°
True anomaly
16.64516°
Mean anomaly
16.5797°
Eccentric anomaly
16.61241°
Mean motion
3.50537 °/min
Orbital period
102.7 mins
BSTAR
0.000081384
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-17 16:25:21.977Z | 154.56° SSE | 2026-05-17 16:29:21.977Z | 110.112° ESE | 22.621° | 2026-05-17 16:34:21.977Z | 50.474° ENE |
| 9 mins | 2026-05-17 18:10:21.977Z | 231.597° WSW | 2026-05-17 18:14:21.977Z | 290.221° WNW | 35.882° | 2026-05-17 18:19:21.977Z | 9.896° NNE |
| 5 mins | 2026-05-18 01:26:21.977Z | 22.663° NE | 2026-05-18 01:28:21.977Z | 45.571° ENE | 15.981° | 2026-05-18 01:31:21.977Z | 79.027° E |
| 10 mins | 2026-05-18 03:10:21.977Z | 334.415° NNW | 2026-05-18 03:14:21.977Z | 292.004° WNW | 44.877° | 2026-05-18 03:20:21.977Z | 159.104° S |
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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