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: 5 hours ago
TLE from 5 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A 26252.90409895 .00006037 00000-0 83221-3 0 9995
2 02826 69.9163 190.4848 0004217 274.5908 85.4758 14.78665537 78753TLE epoch observation values (Epoch: 2026-09-09T21:41:54.149Z)
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
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-10 06:21:38.543Z | 0.283° NNE | 2026-09-10 06:24:38.543Z | 51.009° ENE | 31.747° | 2026-09-10 06:28:38.543Z | 119.917° SE |
| 5 mins | 2026-09-10 08:02:38.543Z | 287.952° WNW | 2026-09-10 08:04:38.543Z | 249.309° W | 24.398° | 2026-09-10 08:07:38.543Z | 204.041° SW |
| 6 mins | 2026-09-10 20:33:38.543Z | 156.133° SSE | 2026-09-10 20:36:38.543Z | 100.724° ESE | 28.403° | 2026-09-10 20:39:38.543Z | 52.146° ENE |
| 6 mins | 2026-09-10 22:13:38.543Z | 258.027° W | 2026-09-10 22:15:38.543Z | 294.7° NW | 27.653° | 2026-09-10 22:19:38.543Z | 0.598° NNE |
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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