OPS 5712 (P/L 152), 2873
Orbit data source: Space-Track
OPS 5712 (P/L 152), 2873 is an American payload satellite in LEO that was launched on Wed, 31 May 1967 UTC via a THOR SLV-2 AGENA D 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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2873 intel report (Beta)
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TLE from 10 hours ago
0 OPS 5712 (P/L 152)
1 02873U 67053G 25199.56861137 .00000047 00000-0 70351-4 0 9995
2 02873 69.9742 47.0784 0009687 238.8230 156.1335 13.98423979961875
TLE epoch observation values (Epoch: 2025-07-18T13:38:48.022Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
OPS 5712 (P/L 152) Visibility forecast
Observer location: undefined°, undefined°
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. |
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10 mins | 2025-07-19 00:19:53.281Z | 349.349° N | 2025-07-19 00:24:53.281Z | 56.737° ENE | 35.062° | 2025-07-19 00:29:53.281Z | 128.641° SE |
8 mins | 2025-07-19 02:06:53.281Z | 300.602° NW | 2025-07-19 02:09:53.281Z | 260.916° W | 24.401° | 2025-07-19 02:14:53.281Z | 201.845° SSW |
4 mins | 2025-07-19 13:39:53.281Z | 116.701° SE | 2025-07-19 13:41:53.281Z | 95.199° ESE | 13.403° | 2025-07-19 13:43:53.281Z | 74.433° E |
10 mins | 2025-07-19 15:21:53.281Z | 208.243° SW | 2025-07-19 15:25:53.281Z | 246.573° WSW | 44.221° | 2025-07-19 15:31:53.281Z | 22.478° NNE |
4 mins | 2025-07-19 17:10:53.281Z | 295.237° NW | 2025-07-19 17:12:53.281Z | 317.204° NNW | 14.075° | 2025-07-19 17:14:53.281Z | 338.567° 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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