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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GGSE 5
1 02834U 67053D 26297.19559265 -.00000002 00000-0 36925-4 0 9998
2 02834 69.9728 216.8049 0006004 20.0699 340.0642 13.96203607 24154Epoch: 2026-10-24T04:41Z
TLE epoch observation values (Epoch: 2026-10-24T04:41:39.204Z)
Latitude
-0.00001°
Longitude
113.78628°
Altitude
905.17 km
Speed
7.402 km/s
True Right ascension
14h 27m 13s
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
08:44:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.39 km
Perigee altitude
900.644 km
Semi-major axis
7,283.154 km
Eccentricity
0.0006
Inclination
69.9728°
RAAN
216.8049°
Arg. of periapsis
20.0699°
True anomaly
340.04072°
Mean anomaly
340.0642°
Eccentric anomaly
340.05246°
Mean motion
3.49192 °/min
Orbital period
103.1 mins
BSTAR
0.000036925
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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 | 2026-10-25 18:38:53.344Z | 136.308° SSE | 2026-10-25 18:41:53.344Z | 103.434° ESE | 18.177° | 2026-10-25 18:45:53.344Z | 60.108° ENE |
| 10 mins | 2026-10-25 20:22:53.344Z | 219.093° SW | 2026-10-25 20:26:53.344Z | 282.24° WNW | 63.589° | 2026-10-25 20:32:53.344Z | 18.493° NNE |
| 4 mins | 2026-10-26 03:40:53.344Z | 27.329° NE | 2026-10-26 03:42:53.344Z | 48.588° ENE | 13.368° | 2026-10-26 03:44:53.344Z | 68.905° E |
| 10 mins | 2026-10-26 05:24:53.344Z | 341.564° N | 2026-10-26 05:28:53.344Z | 39.799° NE | 72.438° | 2026-10-26 05:34:53.344Z | 149.489° SSE |
| 5 mins | 2026-10-26 07:11:53.344Z | 284.866° WNW | 2026-10-26 07:13:53.344Z | 262.921° W | 15.633° | 2026-10-26 07:16:53.344Z | 230.865° 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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