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: 17 hours ago
TLE from 17 hours ago
0 SECOR 3
1 01208U 65016E 26127.82505794 .00000039 00000-0 66510-4 0 9991
2 01208 70.0794 270.0669 0018671 144.7925 331.9849 13.96074485113532TLE epoch observation values (Epoch: 2026-05-07T19:48:05.006Z)
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-08 12:38:14.609Z | 273.75° WNW | 2026-05-08 12:42:14.609Z | 317.398° NNW | 16.509° | 2026-05-08 12:45:14.609Z | 349.255° N |
| 9 mins | 2026-05-08 19:53:14.609Z | 353.086° N | 2026-05-08 19:57:14.609Z | 56.069° ENE | 36.051° | 2026-05-08 20:02:14.609Z | 130.664° SE |
| 8 mins | 2026-05-08 21:39:14.609Z | 301.152° NW | 2026-05-08 21:42:14.609Z | 263.675° W | 22.967° | 2026-05-08 21:47:14.609Z | 204.635° SW |
| 5 mins | 2026-05-09 09:13:14.609Z | 122.53° SE | 2026-05-09 09:15:14.609Z | 100.544° ESE | 15.057° | 2026-05-09 09:18:14.609Z | 68.507° E |
| 9 mins | 2026-05-09 10:56:14.609Z | 213.252° SW | 2026-05-09 11:00:14.609Z | 292.865° NW | 43.838° | 2026-05-09 11:05:14.609Z | 19.593° NNE |
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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