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
Defense Technology
Bus & Motor
NRL 24", Unknown motor
Mass
59 kg wet, 59 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere + 3 Ant, 15.5 m
Radar Cross Section
2.515 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GGSE 3
1 01292U 65016C 25261.16531745 .00000148 00000-0 13266-3 0 9994
2 01292 70.0774 176.4095 0021961 305.8455 54.0614 14.01464342 86454Epoch: 2025-09-18T03:58Z
TLE epoch observation values (Epoch: 2025-09-18T03:58:03.427Z)
Latitude
-0.00002°
Longitude
119.56439°
Altitude
881.708 km
Speed
7.416 km/s
True Right ascension
11h 45m 38s
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
08:20:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.713 km
Perigee altitude
870.804 km
Semi-major axis
7,264.896 km
Eccentricity
0.0022
Inclination
70.0774°
RAAN
176.4095°
Arg. of periapsis
305.8455°
True anomaly
54.26548°
Mean anomaly
54.0614°
Eccentric anomaly
54.16341°
Mean motion
3.50509 °/min
Orbital period
102.71 mins
BSTAR
0.00013266
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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 | 2025-09-18 19:29:27.140Z | 186.25° SSW | 2025-09-18 19:34:27.140Z | 125.203° SE | 40.071° | 2025-09-18 19:40:27.140Z | 32.419° NE |
| 7 mins | 2025-09-18 21:17:27.140Z | 270.021° WNW | 2025-09-18 21:20:27.140Z | 309.029° NW | 21.335° | 2025-09-18 21:24:27.140Z | 355.822° N |
| 9 mins | 2025-09-19 04:30:27.140Z | 0.09° NNE | 2025-09-19 04:34:27.140Z | 55.016° ENE | 28.723° | 2025-09-19 04:39:27.140Z | 117.886° SE |
| 9 mins | 2025-09-19 06:15:27.140Z | 314.3° NW | 2025-09-19 06:19:27.140Z | 260.464° W | 31.519° | 2025-09-19 06:24:27.140Z | 191.242° 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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