OPS 2366 (TRANSIT 14), 2401
Orbit data source: Space-Track
OPS 2366 (TRANSIT 14), 2401 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Thu, 18 Aug 1966 UTC via an SCOUT A 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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2401 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A 26305.24793160 .00000115 00000-0 15218-3 0 9997
2 02401 88.8527 49.7467 0030758 266.1704 121.5396 13.53978452969641TLE epoch observation values (Epoch: 2026-11-01T05:57:01.290Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #76 in the year 1966 (1966-08-18 UTC)
OPS 2366 (TRANSIT 14) 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 | 2026-11-01 18:49:40.616Z | 14.616° NNE | 2026-11-01 18:55:40.616Z | 98.6° ESE | 48.137° | 2026-11-01 19:00:40.616Z | 156.908° SSE |
| 8 mins | 2026-11-01 20:37:40.616Z | 324.647° NNW | 2026-11-01 20:40:40.616Z | 290.142° WNW | 26.436° | 2026-11-01 20:45:40.616Z | 234.13° WSW |
| 11 mins | 2026-11-02 06:45:40.616Z | 143.152° SSE | 2026-11-02 06:50:40.616Z | 79.575° E | 40.955° | 2026-11-02 06:56:40.616Z | 14.192° NNE |
| 10 mins | 2026-11-02 08:32:40.616Z | 225.551° WSW | 2026-11-02 08:36:40.616Z | 273.03° WNW | 31.625° | 2026-11-02 08:42:40.616Z | 338.815° N |
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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