OPS 1264 (DMSP 4A F4), 2980
Orbit data source: Space-Track
OPS 1264 (DMSP 4A F4), 2980 is a payload satellite owned by SAMSO (US) in SSO that was launched on Wed, 11 Oct 1967 UTC via a THOR BURNER 2 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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2980 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OPS 1264 (DMSP 4A F4)
1 02980U 67096A 26094.18038652 .00000784 00000-0 15600-3 0 9995
2 02980 99.1855 161.7357 0092775 337.5245 22.1901 14.62920624 76304TLE epoch observation values (Epoch: 2026-04-04T04:19:45.395Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #96 in the year 1967 (1967-10-11 UTC)
OPS 1264 (DMSP 4A F4) 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 | 2026-04-04 16:25:01.070Z | 52.391° ENE | 2026-04-04 16:28:01.070Z | 97.319° ESE | 21.249° | 2026-04-04 16:31:01.070Z | 140.538° SSE |
| 7 mins | 2026-04-04 18:02:01.070Z | 350.733° N | 2026-04-04 18:05:01.070Z | 297.32° NW | 32.448° | 2026-04-04 18:09:01.070Z | 226.993° WSW |
| 5 mins | 2026-04-05 03:29:01.070Z | 94.126° ESE | 2026-04-05 03:31:01.070Z | 55.301° ENE | 21.289° | 2026-04-05 03:34:01.070Z | 14.033° NNE |
| 6 mins | 2026-04-05 05:05:01.070Z | 209.778° SW | 2026-04-05 05:08:01.070Z | 273.462° WNW | 27.579° | 2026-04-05 05:11:01.070Z | 321.308° NNW |
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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