OPS 5712 (P/L 160), 2826
Orbit data source: Space-Track
OPS 5712 (P/L 160), 2826 is a payload satellite owned by NRL (US) 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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2826 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A 25242.11878772 .00013653 00000-0 21999-2 0 9995
2 02826 69.9207 28.6095 0001008 70.9754 289.1500 14.71588659 23312
TLE epoch observation values (Epoch: 2025-08-30T02:51:03.258Z)
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 160) 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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5 mins | 2025-08-31 09:59:06.785Z | 133.373° SE | 2025-08-31 10:01:06.785Z | 104.762° ESE | 15.976° | 2025-08-31 10:04:06.785Z | 63.814° ENE |
7 mins | 2025-08-31 11:38:06.785Z | 232.471° WSW | 2025-08-31 11:41:06.785Z | 305.239° NW | 36.4° | 2025-08-31 11:45:06.785Z | 12.156° NNE |
7 mins | 2025-08-31 20:11:06.785Z | 353.668° N | 2025-08-31 20:14:06.785Z | 47.01° ENE | 34.306° | 2025-08-31 20:18:06.785Z | 129.685° SE |
4 mins | 2025-08-31 21:53:06.785Z | 275.124° WNW | 2025-08-31 21:54:06.785Z | 258.917° W | 17.289° | 2025-08-31 21:57:06.785Z | 216.592° SW |
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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