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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Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GGSE 5
1 02834U 67053D 26125.68534433 .00000038 00000-0 66677-4 0 9997
2 02834 69.9733 224.0571 0010179 265.5322 94.4620 13.96186392 216TLE epoch observation values (Epoch: 2026-05-05T16:26:53.750Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-06 08:05:02.313Z | 206.335° SW | 2026-05-06 08:08:02.313Z | 359.158° N | 44.69° | 2026-05-06 08:13:02.313Z | 23.596° NE |
| 5 mins | 2026-05-06 09:52:02.313Z | 289.328° WNW | 2026-05-06 09:54:02.313Z | 311.21° NW | 15.014° | 2026-05-06 09:57:02.313Z | 343.554° N |
| 11 mins | 2026-05-06 17:04:02.313Z | 344.007° N | 2026-05-06 17:10:02.313Z | 72.178° E | 39.169° | 2026-05-06 17:15:02.313Z | 137.592° SSE |
| 7 mins | 2026-05-06 18:52:02.313Z | 294.145° NW | 2026-05-06 18:55:02.313Z | 256.719° W | 20.409° | 2026-05-06 18:59:02.313Z | 212.477° SW |
| 6 mins | 2026-05-07 06:25:02.313Z | 128.584° SE | 2026-05-07 06:27:02.313Z | 105.578° ESE | 17.355° | 2026-05-07 06:31:02.313Z | 61.509° ENE |
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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