OPS 1593 (TRANSIT 11), 1952
Orbit data source: Space-Track
OPS 1593 (TRANSIT 11), 1952 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 28 Jan 1966 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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1952 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 1593 (TRANSIT 11)
1 01952U 66005A 25357.23287902 .00000152 00000-0 14233-3 0 9993
2 01952 90.1468 349.0904 0217004 183.4545 176.5132 13.68066491982097TLE epoch observation values (Epoch: 2025-12-23T05:35:20.747Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #5 in the year 1966 (1966-01-28 UTC)
OPS 1593 (TRANSIT 11) 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-23 13:13:18.087Z | 333.356° NNW | 2025-12-23 13:17:18.087Z | 288.036° WNW | 21.093° | 2025-12-23 13:21:18.087Z | 238.848° WSW |
| 10 mins | 2025-12-23 23:16:18.087Z | 140.932° SSE | 2025-12-23 23:21:18.087Z | 73.266° E | 34.351° | 2025-12-23 23:26:18.087Z | 15.174° NNE |
| 10 mins | 2025-12-24 01:01:18.087Z | 221.196° SW | 2025-12-24 01:06:18.087Z | 279.239° WNW | 28.343° | 2025-12-24 01:11:18.087Z | 333.886° NNW |
| 9 mins | 2025-12-24 12:03:18.087Z | 0.812° NNE | 2025-12-24 12:07:18.087Z | 258.293° W | 44.898° | 2025-12-24 12:12:18.087Z | 186.22° 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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