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: 7 hours ago
TLE from 7 hours ago
0 GGSE 3
1 01292U 65016C 25352.23515895 .00000126 00000-0 11833-3 0 9995
2 01292 70.0777 340.6540 0020372 198.4067 161.6307 14.01516608 99212Epoch: 2025-12-18T05:38Z
TLE epoch observation values (Epoch: 2025-12-18T05:38:37.733Z)
Latitude
-0.00005°
Longitude
168.90318°
Altitude
904.926 km
Speed
7.393 km/s
True Right ascension
22h 42m 36s
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
11:30:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
901.378 km
Perigee altitude
871.778 km
Semi-major axis
7,264.715 km
Eccentricity
0.00204
Inclination
70.0777°
RAAN
340.654°
Arg. of periapsis
198.4067°
True anomaly
161.70409°
Mean anomaly
161.6307°
Eccentric anomaly
161.66741°
Mean motion
3.50522 °/min
Orbital period
102.7 mins
BSTAR
0.00011833
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-19 00:36:06.579Z | 192.603° SSW | 2025-12-19 00:41:06.579Z | 113.487° SE | 43.375° | 2025-12-19 00:46:06.579Z | 29.988° NE |
| 6 mins | 2025-12-19 02:24:06.579Z | 276.329° WNW | 2025-12-19 02:27:06.579Z | 312.782° NW | 18.721° | 2025-12-19 02:30:06.579Z | 347.632° N |
| 9 mins | 2025-12-19 09:37:06.579Z | 358.971° N | 2025-12-19 09:41:06.579Z | 63.223° ENE | 31.839° | 2025-12-19 09:46:06.579Z | 125.35° SE |
| 8 mins | 2025-12-19 11:22:06.579Z | 307.958° NW | 2025-12-19 11:26:06.579Z | 252.111° W | 27.091° | 2025-12-19 11:30:06.579Z | 200.618° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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