SECOR 3, 1208
Orbit data source: Space-Track
SECOR 3, 1208 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D 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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1208 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SECOR 3
1 1208U 65016E 26091.14823715 .00000062 00000-0 83559-4 0 9990
2 1208 70.0819 348.1876 0020812 194.2944 318.2710 13.96068031108414TLE epoch observation values (Epoch: 2026-04-01T03:33:27.689Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
SECOR 3 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 | 2026-04-01 18:25:08.745Z | 197.645° SSW | 2026-04-01 18:30:08.745Z | 156.587° SSE | 44.161° | 2026-04-01 18:36:08.745Z | 26.888° NE |
| 6 mins | 2026-04-01 20:14:08.745Z | 280.708° WNW | 2026-04-01 20:17:08.745Z | 315.496° NNW | 17.288° | 2026-04-01 20:20:08.745Z | 348.166° N |
| 9 mins | 2026-04-02 03:28:08.745Z | 352.69° N | 2026-04-02 03:32:08.745Z | 49.601° ENE | 35.19° | 2026-04-02 03:37:08.745Z | 128.326° SE |
| 8 mins | 2026-04-02 05:14:08.745Z | 303.741° NW | 2026-04-02 05:18:08.745Z | 251.19° W | 23.82° | 2026-04-02 05:22:08.745Z | 205.118° SW |
| 4 mins | 2026-04-02 16:49:08.745Z | 113.328° SE | 2026-04-02 16:50:08.745Z | 102.252° ESE | 14.591° | 2026-04-02 16:53:08.745Z | 70.422° E |
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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