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). Payloads include a variety of satellites, spacecraft, and rockets 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)
OV1-9 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | GD/Convair |
| Mission | Defense Technology |
| Bus & Motor | OV1, Unknown motor |
| Mass | 106 kg wet, 106 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Domed Cyl, 1.4 m |
| Radar Cross Section | 0.946 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 OV1-9
1 02610U 66111A 24355.68493762 .00000897 00000-0 35940-3 0 9996
2 02610 99.1016 35.7814 2276181 128.2549 254.6131 10.38894410176568Epoch: 2024-12-20T16:26Z
Definitive object data (Epoch: 2024-12-20T16:26:18.61Z)
| Latitude | 0.00003° |
| Longitude | 59.45695° |
| Altitude | 3,413.661 km |
| Speed | 6.042 km/s |
| True Right ascension | 02h 23m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -29.99882° |
| Longitude | 65.21693° |
| Altitude | 4,279.299 km |
| Speed | 5.469 km/s |
| Apparent Right ascension | 01h 49m 44s |
| Apparent Declination | -35° 10' 54" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:00:20 |
| Azimuth | 273.643° WNW |
| Elevation | -67.897° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 4,510.23 km |
| Perigee altitude | 472.509 km |
| Semi-major axis | 8,869.507 km |
| Eccentricity | 0.2276181 |
| Inclination | 99.1016° |
| RAAN | 35.7814° |
| Arg. of periapsis | 128.2549° |
| True anomaly | 231.84089° |
| Mean anomaly | 254.6131° |
| Eccentric anomaly | 242.99364° |
| Mean motion | 2.59833 °/min |
| BSTAR | 0.0003594 |
| Orbital period | 138.55 mins |
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Other satellites on launch #111 in the year 1966 (1966-12-11 UTC)
| OV1-9, 2610 |
| OV1-10, 2611 (Decayed) |
| OV1-10 R/B, 2621 |
| OV1-9 R/B, 2622 |
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-21 16:13:26.986Z | 354.692° N | 2024-12-21 16:15:26.986Z | 302.853° NW | 34.306° | 2024-12-21 16:18:26.986Z | 217.729° SW |
| 14 mins | 2024-12-22 00:57:26.986Z | 113.404° SE | 2024-12-22 01:05:26.986Z | 71.173° E | 23.747° | 2024-12-22 01:11:26.986Z | 17.741° NNE |
| 21 mins | 2024-12-22 03:08:26.986Z | 175.309° S | 2024-12-22 03:22:26.986Z | 260.07° W | 42.335° | 2024-12-22 03:29:26.986Z | 336.671° NNW |
Authenticating...
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