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 | 16 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 16 hours ago
0 OV1-9
1 02610U 66111A 25044.95345288 .00001247 00000-0 49523-3 0 9993
2 02610 99.0952 66.2449 2276606 43.8100 332.2513 10.39019230182302Epoch: 2025-02-13T22:52Z
Definitive object data (Epoch: 2025-02-13T22:52:58.328Z)
| Latitude | -0.00011° |
| Longitude | -61.22029° |
| Altitude | 846.612 km |
| Speed | 8.09 km/s |
| True Right ascension | 04h 24m 58s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -74.9342° |
| Longitude | -24.53584° |
| Altitude | 3,165.01 km |
| Speed | 6.224 km/s |
| Apparent Right ascension | 05h 47m 50s |
| Apparent Declination | -61° 22' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:15:44 |
| Azimuth | 190.28° SSW |
| Elevation | -67.989° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 4,509.734 km |
| Perigee altitude | 471.583 km |
| Semi-major axis | 8,868.796 km |
| Eccentricity | 0.2276606 |
| Inclination | 99.0952° |
| RAAN | 66.2449° |
| Arg. of periapsis | 43.81° |
| True anomaly | 316.30376° |
| Mean anomaly | 332.2513° |
| Eccentric anomaly | 324.71686° |
| Mean motion | 2.59864 °/min |
| BSTAR | 0.00049523 |
| Orbital period | 138.53 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. |
|---|---|---|---|---|---|---|---|
| 20 mins | 2025-02-14 15:32:44.895Z | 350.906° N | 2025-02-14 15:39:44.895Z | 288.621° WNW | 32.915° | 2025-02-14 15:52:44.895Z | 231.404° WSW |
| 22 mins | 2025-02-15 12:23:44.895Z | 47.456° ENE | 2025-02-15 12:31:44.895Z | 103.185° ESE | 27.835° | 2025-02-15 12:45:44.895Z | 155.783° SSE |
Authenticating...
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