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: 1 day ago
TLE from 1 day ago
0 GGSE 3
1 01292U 65016C 25315.26520076 .00000335 00000-0 25612-3 0 9996
2 01292 70.0780 60.1224 0022127 242.7286 117.1569 14.01496209 94030Epoch: 2025-11-11T06:21Z
TLE epoch observation values (Epoch: 2025-11-11T06:21:53.345Z)
Latitude
-0.00008°
Longitude
-86.00414°
Altitude
898.31 km
Speed
7.399 km/s
True Right ascension
04h 00m 29s
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
02:22:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.723 km
Perigee altitude
870.574 km
Semi-major axis
7,264.786 km
Eccentricity
0.00221
Inclination
70.078°
RAAN
60.1224°
Arg. of periapsis
242.7286°
True anomaly
117.38222°
Mean anomaly
117.1569°
Eccentric anomaly
117.26959°
Mean motion
3.50517 °/min
Orbital period
102.71 mins
BSTAR
0.00025612
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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 | 2025-11-12 08:10:03.890Z | 189.092° SSW | 2025-11-12 08:15:03.890Z | 128.068° SE | 41.584° | 2025-11-12 08:21:03.890Z | 30.987° NE |
| 7 mins | 2025-11-12 09:58:03.890Z | 271.695° WNW | 2025-11-12 10:01:03.890Z | 308.944° NW | 20.349° | 2025-11-12 10:05:03.890Z | 354.757° N |
| 9 mins | 2025-11-12 17:11:03.890Z | 358.642° N | 2025-11-12 17:15:03.890Z | 54.976° ENE | 30.047° | 2025-11-12 17:20:03.890Z | 120.378° SE |
| 9 mins | 2025-11-12 18:56:03.890Z | 312.533° NW | 2025-11-12 19:00:03.890Z | 259.587° W | 29.566° | 2025-11-12 19:05:03.890Z | 193.668° SSW |
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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