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: 14 hours ago
TLE from 14 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26080.49729041 .00000088 00000-0 15391-3 0 9993
2 01514 89.9895 227.9276 0071155 48.9141 20.1412 13.35353466949564TLE epoch observation values (Epoch: 2026-03-21T11:56:05.891Z)
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 | 2026-03-22 09:17:09.544Z | 141.297° SSE | 2026-03-22 09:22:09.544Z | 86.58° E | 31.447° | 2026-03-22 09:28:09.544Z | 15.302° NNE |
| 9 mins | 2026-03-22 11:06:09.544Z | 224.156° SW | 2026-03-22 11:10:09.544Z | 275.872° WNW | 28.707° | 2026-03-22 11:15:09.544Z | 334.468° NNW |
| 7 mins | 2026-03-22 20:36:09.544Z | 49.393° ENE | 2026-03-22 20:39:09.544Z | 80.599° E | 18.25° | 2026-03-22 20:43:09.544Z | 118.348° SE |
| 11 mins | 2026-03-22 22:22:09.544Z | 354.52° N | 2026-03-22 22:27:09.544Z | 276.176° WNW | 43.103° | 2026-03-22 22:33:09.544Z | 195.568° 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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