GGSE 5, 2834
Orbit data source: Space-Track
GGSE 5, 2834 is an American payload satellite in LEO that was launched on Wed, 31 May 1967 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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2834 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL MULTI, Unknown motor
Mass
105 kg wet, 105 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
ELL + 2 ANT, 9.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GGSE 5
1 02834U 67053D 26230.71233613 .00000008 00000-0 44247-4 0 9990
2 02834 69.9747 359.1665 0005517 145.1774 214.9694 13.96197323 14872Epoch: 2026-08-18T17:05Z
TLE epoch observation values (Epoch: 2026-08-18T17:05:45.841Z)
Latitude
0.00001°
Longitude
135.64928°
Altitude
912.599 km
Speed
7.394 km/s
True Right ascension
23h 56m 39s
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
23:23:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.057 km
Perigee altitude
901.02 km
Semi-major axis
7,283.176 km
Eccentricity
0.00055
Inclination
69.9747°
RAAN
359.1665°
Arg. of periapsis
145.1774°
True anomaly
214.93319°
Mean anomaly
214.9694°
Eccentric anomaly
214.95129°
Mean motion
3.4919 °/min
Orbital period
103.1 mins
BSTAR
0.000044247
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Other satellites on launch #53 in the year 1967 (1967-05-31 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 5 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-19 08:42:15.108Z | 133.245° SE | 2026-08-19 08:45:15.108Z | 99.2° ESE | 17.299° | 2026-08-19 08:48:15.108Z | 65.706° ENE |
| 9 mins | 2026-08-19 10:26:15.108Z | 219.94° SW | 2026-08-19 10:30:15.108Z | 301.166° NW | 42.127° | 2026-08-19 10:35:15.108Z | 17.23° NNE |
| 10 mins | 2026-08-19 19:27:15.108Z | 340.347° N | 2026-08-19 19:32:15.108Z | 74.151° E | 43.805° | 2026-08-19 19:37:15.108Z | 148.631° SSE |
| 5 mins | 2026-08-19 21:15:15.108Z | 281.033° WNW | 2026-08-19 21:17:15.108Z | 258.431° W | 14.892° | 2026-08-19 21:20:15.108Z | 227.466° WSW |
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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