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: 19 hours ago
TLE from 19 hours ago
0 GGSE 3
1 01292U 65016C 25321.61721742 .00000242 00000-0 19498-3 0 9997
2 01292 70.0787 46.4695 0021980 235.3952 124.5085 14.01501213 94925Epoch: 2025-11-17T14:48Z
TLE epoch observation values (Epoch: 2025-11-17T14:48:47.585Z)
Latitude
0.00007°
Longitude
127.35617°
Altitude
899.999 km
Speed
7.398 km/s
True Right ascension
03h 05m 52s
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
06:31:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.599 km
Perigee altitude
870.663 km
Semi-major axis
7,264.768 km
Eccentricity
0.0022
Inclination
70.0787°
RAAN
46.4695°
Arg. of periapsis
235.3952°
True anomaly
124.71573°
Mean anomaly
124.5085°
Eccentric anomaly
124.61215°
Mean motion
3.50518 °/min
Orbital period
102.71 mins
BSTAR
0.00019498
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-18 15:20:07.486Z | 5.114° NNE | 2025-11-18 15:24:07.486Z | 49.363° ENE | 18.945° | 2025-11-18 15:28:07.486Z | 94.319° ESE |
| 10 mins | 2025-11-18 17:05:07.486Z | 329.193° NNW | 2025-11-18 17:10:07.486Z | 234.728° WSW | 42.894° | 2025-11-18 17:15:07.486Z | 168.047° S |
| 9 mins | 2025-11-19 06:20:07.486Z | 166.197° S | 2025-11-19 06:24:07.486Z | 104.826° ESE | 32.757° | 2025-11-19 06:29:07.486Z | 40.846° NE |
| 9 mins | 2025-11-19 08:05:07.486Z | 248.288° W | 2025-11-19 08:09:07.486Z | 300.494° NW | 27.746° | 2025-11-19 08:14:07.486Z | 4.033° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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