OPS 8464 (TRANSIT 5B-7), 1514
Orbit data source: Space-Track
OPS 8464 (TRANSIT 5B-7), 1514 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 13 Aug 1965 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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1514 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26061.54006906 .00000094 00000-0 16436-3 0 9994
2 01514 89.9860 227.9485 0071836 101.0699 328.9960 13.35350056947032TLE epoch observation values (Epoch: 2026-03-02T12:57:41.966Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)
OPS 8464 (TRANSIT 5B-7) 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-03-03 10:18:27.827Z | 134.976° SE | 2026-03-03 10:24:27.827Z | 72.243° E | 27.023° | 2026-03-03 10:29:27.827Z | 20.32° NNE |
| 11 mins | 2026-03-03 12:06:27.827Z | 208.804° SW | 2026-03-03 12:11:27.827Z | 271.045° WNW | 34.062° | 2026-03-03 12:17:27.827Z | 342.477° N |
| 4 mins | 2026-03-03 21:38:27.827Z | 59.523° ENE | 2026-03-03 21:40:27.827Z | 78.98° E | 13.665° | 2026-03-03 21:42:27.827Z | 97.832° ESE |
| 11 mins | 2026-03-03 23:23:27.827Z | 0.777° NNE | 2026-03-03 23:28:27.827Z | 310.533° NW | 44.864° | 2026-03-03 23:34:27.827Z | 186.419° SSW |
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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