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: 9 hours ago
TLE from 9 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 1514U 65065F 26170.72375507 .00000082 00000-0 14054-3 0 9992
2 1514 89.9965 227.8978 0071272 152.0809 328.7809 13.35371112961602TLE epoch observation values (Epoch: 2026-06-19T17:22:12.438Z)
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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-06-20 03:39:16.819Z | 155.049° SSE | 2026-06-20 03:45:16.819Z | 95.752° ESE | 38.324° | 2026-06-20 03:52:16.819Z | 7.934° NNE |
| 9 mins | 2026-06-20 05:29:16.819Z | 232.212° WSW | 2026-06-20 05:33:16.819Z | 273.594° WNW | 23.562° | 2026-06-20 05:38:16.819Z | 327.227° NNW |
| 9 mins | 2026-06-20 14:58:16.819Z | 33.982° NE | 2026-06-20 15:02:16.819Z | 76.983° E | 22.864° | 2026-06-20 15:07:16.819Z | 131.021° SE |
| 11 mins | 2026-06-20 16:45:16.819Z | 348.181° N | 2026-06-20 16:50:16.819Z | 284.815° WNW | 37.553° | 2026-06-20 16:56:16.819Z | 207.141° 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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