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: 17 hours ago
TLE from 17 hours ago
0 OPS 6582 (TRANSIT 5B-5)
1 00965U 64083D 26202.47299192 .00000059 00000-0 69971-4 0 9996
2 00965 90.0762 203.3136 0041718 174.6944 338.0707 13.57015535 48263TLE epoch observation values (Epoch: 2026-07-21T11:21:06.501Z)
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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-07-22 11:57:57.677Z | 12.162° NNE | 2026-07-22 12:03:57.677Z | 88.256° E | 38.955° | 2026-07-22 12:09:57.677Z | 164.901° S |
| 8 mins | 2026-07-22 13:45:57.677Z | 325.195° NNW | 2026-07-22 13:48:57.677Z | 291.884° WNW | 20.999° | 2026-07-22 13:53:57.677Z | 238.363° WSW |
| 11 mins | 2026-07-22 23:52:57.677Z | 150.687° SSE | 2026-07-22 23:57:57.677Z | 78.911° E | 38.051° | 2026-07-23 00:03:57.677Z | 8.645° NNE |
| 9 mins | 2026-07-23 01:39:57.677Z | 232.959° WSW | 2026-07-23 01:43:57.677Z | 277.246° WNW | 22.883° | 2026-07-23 01:48:57.677Z | 329.892° 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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