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: 19 hours ago
TLE from 19 hours ago
0 OPS 0100 (TRANSIT 15)
1 2754U 67034A 26015.61143409 .00000123 00000-0 15953-3 0 9992
2 2754 90.2248 31.5580 0018024 229.1147 245.3748 13.57366786905412TLE epoch observation values (Epoch: 2026-01-15T14:40:27.905Z)
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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-01-16 11:56:55.868Z | 33.018° NE | 2026-01-16 12:01:55.868Z | 83.929° E | 19.695° | 2026-01-16 12:05:55.868Z | 124.491° SE |
| 11 mins | 2026-01-16 13:42:55.868Z | 351.571° N | 2026-01-16 13:47:55.868Z | 276.466° WNW | 40.685° | 2026-01-16 13:53:55.868Z | 200.568° SSW |
| 7 mins | 2026-01-16 23:52:55.868Z | 107.918° ESE | 2026-01-16 23:55:55.868Z | 76.063° E | 19.355° | 2026-01-16 23:59:55.868Z | 33.852° NE |
| 11 mins | 2026-01-17 01:36:55.868Z | 193.886° SSW | 2026-01-17 01:41:55.868Z | 291.187° WNW | 41.223° | 2026-01-17 01:47:55.868Z | 350.939° 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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