GGSE 4, 2828
Orbit data source: Space-Track
GGSE 4, 2828 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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2828 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 GGSE 4
1 2828U 67053C 26130.45328118 .00000058 00000-0 78191-4 0 9998
2 2828 69.9688 143.9936 0009856 230.9149 129.1081 13.98079692 2883TLE epoch observation values (Epoch: 2026-05-10T10:52:43.493Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
GGSE 4 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 | 2026-05-11 00:45:48.105Z | 118.719° SE | 2026-05-11 00:47:48.105Z | 97.53° ESE | 13.382° | 2026-05-11 00:49:48.105Z | 76.495° E |
| 10 mins | 2026-05-11 02:27:48.105Z | 207.783° SW | 2026-05-11 02:32:48.105Z | 346.103° N | 44.181° | 2026-05-11 02:37:48.105Z | 22.378° NNE |
| 5 mins | 2026-05-11 04:16:48.105Z | 292.538° NW | 2026-05-11 04:18:48.105Z | 314.221° NW | 14.178° | 2026-05-11 04:21:48.105Z | 345.408° N |
| 9 mins | 2026-05-11 11:29:48.105Z | 349.469° N | 2026-05-11 11:33:48.105Z | 68.04° E | 40.164° | 2026-05-11 11:38:48.105Z | 139.18° SSE |
| 6 mins | 2026-05-11 13:15:48.105Z | 293.12° NW | 2026-05-11 13:18:48.105Z | 256.405° W | 19.231° | 2026-05-11 13:21:48.105Z | 221.32° SW |
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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