OV1-9, 2610
Orbit data source: Space-Track
OV1-9, 2610 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Sun, 11 Dec 1966 UTC via an ATLAS 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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2610 intel report (Beta)
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TLE from 1 day ago
0 OV1-9
1 02610U 66111A 25199.45311353 .00000289 00000-0 12096-3 0 9995
2 02610 99.1022 151.5526 2274410 167.6205 199.2010 10.39340765198352
TLE epoch observation values (Epoch: 2025-07-18T10:52:29.008Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)
OV1-9 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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11 mins | 2025-07-19 17:17:07.576Z | 70.164° E | 2025-07-19 17:23:07.576Z | 48.438° ENE | 13.173° | 2025-07-19 17:28:07.576Z | 25.113° NE |
30 mins | 2025-07-19 19:18:07.576Z | 133.247° SE | 2025-07-19 19:37:07.576Z | 64.133° ENE | 38.9° | 2025-07-19 19:48:07.576Z | 357.606° N |
34 mins | 2025-07-19 21:31:07.576Z | 184.535° SSW | 2025-07-19 21:52:07.576Z | 260.636° W | 39.806° | 2025-07-19 22:05:07.576Z | 335.466° NNW |
9 mins | 2025-07-20 00:04:07.576Z | 261.333° W | 2025-07-20 00:08:07.576Z | 273.382° WNW | 11.44° | 2025-07-20 00:13:07.576Z | 290.254° WNW |
6 mins | 2025-07-20 09:56:07.576Z | 6.416° NNE | 2025-07-20 09:59:07.576Z | 295.866° NW | 42.555° | 2025-07-20 10:02:07.576Z | 206.29° 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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