OPS 0100 (TRANSIT 15), 2754
Orbit data source: Space-Track
OPS 0100 (TRANSIT 15), 2754 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Fri, 14 Apr 1967 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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2754 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 26304.72684522 .00000101 00000-0 12862-3 0 9993
2 02754 90.2458 38.4751 0021553 106.3231 46.4785 13.57429345944631TLE epoch observation values (Epoch: 2026-10-31T17:26:39.427Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)
OPS 0100 (TRANSIT 15) 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 18:03:25.080Z | 18.355° NNE | 2026-11-01 18:09:25.080Z | 98.11° ESE | 42.09° | 2026-11-01 18:14:25.080Z | 154.805° SSE |
| 9 mins | 2026-11-01 19:50:25.080Z | 333.362° NNW | 2026-11-01 19:54:25.080Z | 285.866° WNW | 29.108° | 2026-11-01 19:59:25.080Z | 229.598° WSW |
| 10 mins | 2026-11-02 05:58:25.080Z | 139.502° SSE | 2026-11-02 06:02:25.080Z | 87.966° E | 40.535° | 2026-11-02 06:08:25.080Z | 13.385° NNE |
| 9 mins | 2026-11-02 07:44:25.080Z | 223.917° SW | 2026-11-02 07:48:25.080Z | 271.316° WNW | 30.29° | 2026-11-02 07:53:25.080Z | 331.508° 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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