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: 20 hours ago
TLE from 20 hours ago
0 OPS 0100 (TRANSIT 15)
1 02754U 67034A 25340.89046131 .00000217 00000-0 29157-3 0 9991
2 02754 90.2276 30.6481 0019004 354.7399 179.4568 13.57355120900025TLE epoch observation values (Epoch: 2025-12-06T21:22:15.857Z)
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-08 02:42:35.327Z | 130.814° SE | 2025-12-08 02:47:35.327Z | 78.786° E | 25.035° | 2025-12-08 02:52:35.327Z | 22.949° NE |
| 10 mins | 2025-12-08 04:28:35.327Z | 206.75° SW | 2025-12-08 04:33:35.327Z | 279.006° WNW | 35.034° | 2025-12-08 04:38:35.327Z | 341.272° N |
| 11 mins | 2025-12-08 15:34:35.327Z | 8.469° NNE | 2025-12-08 15:39:35.327Z | 71.912° E | 43.428° | 2025-12-08 15:45:35.327Z | 174.833° S |
| 6 mins | 2025-12-08 17:22:35.327Z | 314.022° NW | 2025-12-08 17:24:35.327Z | 293.086° NW | 16.951° | 2025-12-08 17:28:35.327Z | 253.005° W |
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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