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: 12 hours ago
TLE from 12 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26255.98107208 .00000050 00000-0 82181-4 0 9997
2 01514 89.9996 227.8789 0067859 273.7040 148.9622 13.35380656972981TLE epoch observation values (Epoch: 2026-09-12T23:32:44.627Z)
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-13 12:27:06.516Z | 317.697° NNW | 2026-09-13 12:30:06.516Z | 291.186° WNW | 14.741° | 2026-09-13 12:33:06.516Z | 264.706° W |
| 6 mins | 2026-09-13 20:59:06.516Z | 94.793° ESE | 2026-09-13 21:02:06.516Z | 65.411° ENE | 17.447° | 2026-09-13 21:05:06.516Z | 38.153° NE |
| 12 mins | 2026-09-13 22:43:06.516Z | 182.195° SSW | 2026-09-13 22:48:06.516Z | 239.189° WSW | 78.564° | 2026-09-13 22:55:06.516Z | 355.4° N |
| 11 mins | 2026-09-14 10:01:06.516Z | 16.814° NNE | 2026-09-14 10:06:06.516Z | 84.401° E | 54.047° | 2026-09-14 10:12:06.516Z | 162.041° S |
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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