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: 12 hours ago
TLE from 12 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 26126.49146155 .00000127 00000-0 16515-3 0 9991
2 02754 90.2379 34.1738 0017435 269.4374 264.1441 13.57397017920456TLE epoch observation values (Epoch: 2026-05-06T11:47:42.277Z)
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 | 2026-05-07 05:13:46.107Z | 23.141° NE | 2026-05-07 05:19:46.107Z | 92.329° ESE | 27.925° | 2026-05-07 05:24:46.107Z | 144.701° SSE |
| 10 mins | 2026-05-07 07:00:46.107Z | 339.872° N | 2026-05-07 07:04:46.107Z | 289.668° WNW | 32.065° | 2026-05-07 07:10:46.107Z | 216.633° SW |
| 10 mins | 2026-05-07 17:08:46.107Z | 129.782° SE | 2026-05-07 17:13:46.107Z | 68.615° E | 27.053° | 2026-05-07 17:18:46.107Z | 18.304° NNE |
| 10 mins | 2026-05-07 18:54:46.107Z | 213.975° SW | 2026-05-07 18:58:46.107Z | 269.912° W | 33.276° | 2026-05-07 19:04:46.107Z | 341.929° 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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