OPS 8480 (TRANSIT 5B-6), 1420
Orbit data source: Space-Track
OPS 8480 (TRANSIT 5B-6), 1420 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Thu, 24 Jun 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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1420 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 8480 (TRANSIT 5B-6)
1 1420U 65048A 26035.29606806 .00000151 00000-0 21044-3 0 9994
2 1420 89.8811 287.8640 0075133 95.9369 25.3665 13.51878354985496TLE epoch observation values (Epoch: 2026-02-04T07:06:20.280Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #48 in the year 1965 (1965-06-24 UTC)
OPS 8480 (TRANSIT 5B-6) 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 | 2026-02-05 04:25:17.189Z | 17.338° NNE | 2026-02-05 04:30:17.189Z | 76.288° E | 34.854° | 2026-02-05 04:36:17.189Z | 156.618° SSE |
| 8 mins | 2026-02-05 06:13:17.189Z | 326.94° NNW | 2026-02-05 06:16:17.189Z | 290.667° WNW | 24.416° | 2026-02-05 06:21:17.189Z | 232.779° WSW |
| 10 mins | 2026-02-05 16:23:17.189Z | 143.052° SSE | 2026-02-05 16:27:17.189Z | 91.857° ESE | 34.158° | 2026-02-05 16:33:17.189Z | 13.008° NNE |
| 9 mins | 2026-02-05 18:10:17.189Z | 229.469° WSW | 2026-02-05 18:14:17.189Z | 278.497° WNW | 25.148° | 2026-02-05 18:19:17.189Z | 333.326° NNW |
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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