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: 7 hours ago
TLE from 7 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 26085.27325625 .00000174 00000-0 23076-3 0 9994
2 02754 90.2349 33.1787 0020911 33.7635 83.1553 13.57385993914862TLE epoch observation values (Epoch: 2026-03-26T06:33:29.339Z)
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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-03-26 20:14:07.620Z | 152.828° SSE | 2026-03-26 20:20:07.620Z | 82.722° E | 36.803° | 2026-03-26 20:26:07.620Z | 9.442° NNE |
| 8 mins | 2026-03-26 22:03:07.620Z | 238.89° WSW | 2026-03-26 22:06:07.620Z | 275.786° WNW | 23.103° | 2026-03-26 22:11:07.620Z | 330.154° NNW |
| 7 mins | 2026-03-27 07:23:07.620Z | 48.136° ENE | 2026-03-27 07:26:07.620Z | 80.239° E | 17.692° | 2026-03-27 07:30:07.620Z | 119.646° SE |
| 11 mins | 2026-03-27 09:07:07.620Z | 355.126° N | 2026-03-27 09:12:07.620Z | 292.424° WNW | 42.471° | 2026-03-27 09:18:07.620Z | 196.664° SSW |
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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