OPS 6582 (TRANSIT 5B-5), 965
Orbit data source: Space-Track
OPS 6582 (TRANSIT 5B-5), 965 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Sun, 13 Dec 1964 UTC via a THOR ABLESTAR 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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965 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OPS 6582 (TRANSIT 5B-5)
1 00965U 64083D 26145.62524264 .00000063 00000-0 75165-4 0 9997
2 00965 90.0781 202.8582 0040916 346.7136 177.0236 13.57010575 40558TLE epoch observation values (Epoch: 2026-05-25T15:00:20.964Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #83 in the year 1964 (1964-12-13 UTC)
OPS 6582 (TRANSIT 5B-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 | 2026-05-26 02:43:51.217Z | 111.945° ESE | 2026-05-26 02:47:51.217Z | 72.504° E | 17.402° | 2026-05-26 02:51:51.217Z | 32.763° NE |
| 11 mins | 2026-05-26 04:27:51.217Z | 188.269° SSW | 2026-05-26 04:32:51.217Z | 253.432° W | 42.687° | 2026-05-26 04:38:51.217Z | 351.466° N |
| 11 mins | 2026-05-26 15:34:51.217Z | 18.289° NNE | 2026-05-26 15:39:51.217Z | 87.949° E | 37.127° | 2026-05-26 15:45:51.217Z | 160.644° S |
| 8 mins | 2026-05-26 17:21:51.217Z | 326.72° NNW | 2026-05-26 17:25:51.217Z | 277.881° WNW | 24.044° | 2026-05-26 17:29:51.217Z | 235.909° 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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