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: 5 hours ago
TLE from 5 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 1514U 65065F 26305.22857259 .00000084 00000-0 14384-3 0 9994
2 1514 90.0085 227.9048 0070935 133.2966 22.0050 13.35386046979554TLE epoch observation values (Epoch: 2026-11-01T05:29:08.671Z)
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 | 2026-11-01 19:12:55.212Z | 168.316° S | 2026-11-01 19:17:55.212Z | 93.229° ESE | 77.663° | 2026-11-01 19:23:55.212Z | 1.38° NNE |
| 6 mins | 2026-11-01 21:03:55.212Z | 259.115° W | 2026-11-01 21:05:55.212Z | 278.621° WNW | 16.806° | 2026-11-01 21:09:55.212Z | 316.573° NNW |
| 10 mins | 2026-11-02 06:30:55.212Z | 28.512° NE | 2026-11-02 06:34:55.212Z | 81.771° E | 37.57° | 2026-11-02 06:40:55.212Z | 150.535° SSE |
| 10 mins | 2026-11-02 08:17:55.212Z | 338.137° N | 2026-11-02 08:22:55.212Z | 276.445° WNW | 33.631° | 2026-11-02 08:27:55.212Z | 223.143° 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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