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
SPHERE + 3 ANT, 15.5 m
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 26209.18878006 .00000078 00000-0 86200-4 0 9994
2 1292 70.0747 223.5104 0022099 256.9338 102.9304 14.01598208130311Epoch: 2026-07-28T04:31Z
TLE epoch observation values (Epoch: 2026-07-28T04:31:50.597Z)
Latitude
-0.00004°
Longitude
-150.31202°
Altitude
894.217 km
Speed
7.403 km/s
True Right ascension
14h 54m 02s
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
23:34:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.35 km
Perigee altitude
870.243 km
Semi-major axis
7,264.433 km
Eccentricity
0.00221
Inclination
70.0747°
RAAN
223.5104°
Arg. of periapsis
256.9338°
True anomaly
103.17706°
Mean anomaly
102.9304°
Eccentric anomaly
103.05375°
Mean motion
3.50542 °/min
Orbital period
102.7 mins
BSTAR
0.0000862
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-28 10:13:22.933Z | 22.383° NNE | 2026-07-28 10:15:22.933Z | 42.868° NE | 12.3° | 2026-07-28 10:17:22.933Z | 63.546° ENE |
| 10 mins | 2026-07-28 11:57:22.933Z | 342.712° N | 2026-07-28 12:01:22.933Z | 36.528° NE | 42.783° | 2026-07-28 12:07:22.933Z | 147.61° SSE |
| 5 mins | 2026-07-28 13:44:22.933Z | 282.602° WNW | 2026-07-28 13:46:22.933Z | 259.426° W | 15.71° | 2026-07-28 13:49:22.933Z | 227.172° WSW |
| 7 mins | 2026-07-29 01:13:22.933Z | 136.718° SSE | 2026-07-29 01:16:22.933Z | 97.462° ESE | 20.994° | 2026-07-29 01:20:22.933Z | 53.707° ENE |
| 10 mins | 2026-07-29 02:56:22.933Z | 226.545° WSW | 2026-07-29 03:00:22.933Z | 281.726° WNW | 38.033° | 2026-07-29 03:06:22.933Z | 14.727° 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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