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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GGSE 5
1 02834U 67053D 26083.91788736 .00000040 00000-0 67810-4 0 9996
2 02834 69.9730 313.4958 0009431 305.4484 54.5741 13.96180227994378Epoch: 2026-03-24T22:01Z
TLE epoch observation values (Epoch: 2026-03-24T22:01:45.467Z)
Latitude
-0°
Longitude
160.6677°
Altitude
905.384 km
Speed
7.402 km/s
True Right ascension
20h 53m 58s
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
11:45:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.967 km
Perigee altitude
898.229 km
Semi-major axis
7,283.235 km
Eccentricity
0.00094
Inclination
69.973°
RAAN
313.4958°
Arg. of periapsis
305.4484°
True anomaly
54.66222°
Mean anomaly
54.5741°
Eccentric anomaly
54.61816°
Mean motion
3.49186 °/min
Orbital period
103.1 mins
BSTAR
0.00006781
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-25 15:20:31.377Z | 142.906° SSE | 2026-03-25 15:24:31.377Z | 98.805° ESE | 18.579° | 2026-03-25 15:27:31.377Z | 64.39° ENE |
| 9 mins | 2026-03-25 17:05:31.377Z | 223.34° SW | 2026-03-25 17:09:31.377Z | 301.559° NW | 40.97° | 2026-03-25 17:14:31.377Z | 15.843° NNE |
| 4 mins | 2026-03-26 00:23:31.377Z | 30.444° NE | 2026-03-26 00:24:31.377Z | 41.343° NE | 13.884° | 2026-03-26 00:27:31.377Z | 72.834° E |
| 10 mins | 2026-03-26 02:06:31.377Z | 338.686° N | 2026-03-26 02:11:31.377Z | 73.56° E | 44.488° | 2026-03-26 02:16:31.377Z | 151.491° SSE |
| 4 mins | 2026-03-26 03:54:31.377Z | 280.707° WNW | 2026-03-26 03:56:31.377Z | 259.039° W | 13.891° | 2026-03-26 03:58:31.377Z | 238.02° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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