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: 6 hours ago
TLE from 6 hours ago
0 GGSE 3
1 1292U 65016C 25308.05670487 .00000161 00000-0 14167-3 0 9997
2 1292 70.0766 75.6167 0022261 251.0902 108.7794 14.01491475 93022Epoch: 2025-11-04T01:21Z
TLE epoch observation values (Epoch: 2025-11-04T01:21:39.300Z)
Latitude
-0.00002°
Longitude
11.65374°
Altitude
896.199 km
Speed
7.402 km/s
True Right ascension
05h 02m 28s
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
03:23:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.837 km
Perigee altitude
870.493 km
Semi-major axis
7,264.802 km
Eccentricity
0.00223
Inclination
70.0766°
RAAN
75.6167°
Arg. of periapsis
251.0902°
True anomaly
109.0207°
Mean anomaly
108.7794°
Eccentric anomaly
108.90007°
Mean motion
3.50516 °/min
Orbital period
102.71 mins
BSTAR
0.00014167
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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 | 2025-11-04 10:02:31.151Z | 197.804° SSW | 2025-11-04 10:07:31.151Z | 135.175° SSE | 44.526° | 2025-11-04 10:13:31.151Z | 26.675° NE |
| 5 mins | 2025-11-04 11:51:31.151Z | 287.069° WNW | 2025-11-04 11:53:31.151Z | 310.893° NW | 17.06° | 2025-11-04 11:56:31.151Z | 344.974° N |
| 9 mins | 2025-11-04 19:03:31.151Z | 354.908° N | 2025-11-04 19:07:31.151Z | 57.943° ENE | 34.765° | 2025-11-04 19:12:31.151Z | 128.579° SE |
| 7 mins | 2025-11-04 20:49:31.151Z | 298.456° NW | 2025-11-04 20:52:31.151Z | 256.303° W | 24.624° | 2025-11-04 20:56:31.151Z | 206.174° SW |
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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