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 01292U 65016C 26107.91961688 .00000030 00000-0 54607-4 0 9995
2 01292 70.0757 81.2209 0018184 21.6871 338.5004 14.01567510116125Epoch: 2026-04-17T22:04Z
TLE epoch observation values (Epoch: 2026-04-17T22:04:14.898Z)
Latitude
-0.00003°
Longitude
-95.88708°
Altitude
878.403 km
Speed
7.42 km/s
True Right ascension
05h 24m 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
15:24:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
899.612 km
Perigee altitude
873.193 km
Semi-major axis
7,264.539 km
Eccentricity
0.00182
Inclination
70.0757°
RAAN
81.2209°
Arg. of periapsis
21.6871°
True anomaly
338.42387°
Mean anomaly
338.5004°
Eccentric anomaly
338.46215°
Mean motion
3.50535 °/min
Orbital period
102.7 mins
BSTAR
0.000054607
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-18 08:54:00.554Z | 344.523° N | 2026-04-18 08:59:00.554Z | 51.747° ENE | 40.066° | 2026-04-18 09:05:00.554Z | 141.08° SSE |
| 7 mins | 2026-04-18 10:41:00.554Z | 294.158° NW | 2026-04-18 10:44:00.554Z | 257.811° W | 19.145° | 2026-04-18 10:48:00.554Z | 214.224° SW |
| 5 mins | 2026-04-18 22:12:00.554Z | 123.184° SE | 2026-04-18 22:14:00.554Z | 98.495° ESE | 17.004° | 2026-04-18 22:17:00.554Z | 64.69° ENE |
| 10 mins | 2026-04-18 23:54:00.554Z | 218.637° SW | 2026-04-18 23:58:00.554Z | 272.417° WNW | 41.135° | 2026-04-19 00:04:00.554Z | 17.954° 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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