OV1-10 R/B, 2621
Orbit data source: Space-Track
OV1-10 R/B, 2621 is space debris in LEO originally from a launch on Sun, 11 Dec 1966 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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2621 intel report (Beta)
OV1-10 R/B details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | ABL |
| Mission | Spacecraft |
| Bus & Motor | ALTAIR, Unknown motor |
| Mass | 125 kg wet, 125 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 2.1 m |
| Radar Cross Section | 1.347 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 OV1-10 R/B
1 02621U 66111C 24355.66525291 .00001641 00000-0 19244-3 0 9996
2 02621 93.3972 332.6933 0056763 195.9572 163.9866 14.84041916 93706Epoch: 2024-12-20T15:57Z
Definitive object data (Epoch: 2024-12-20T15:57:57.851Z)
| Latitude | -0.00001° |
| Longitude | 3.47475° |
| Altitude | 657.908 km |
| Speed | 7.508 km/s |
| True Right ascension | 22h 10m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -82.13113° |
| Longitude | 158.5521° |
| Altitude | 631.182 km |
| Speed | 7.549 km/s |
| Apparent Right ascension | 00h 12m 56s |
| Apparent Declination | -68° 41' 17" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:35:41 |
| Azimuth | 186.924° SSW |
| Elevation | -60.793° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 653.171 km |
| Perigee altitude | 573.798 km |
| Semi-major axis | 6,991.622 km |
| Eccentricity | 0.0056763 |
| Inclination | 93.3972° |
| RAAN | 332.6933° |
| Arg. of periapsis | 195.9572° |
| True anomaly | 164.16482° |
| Mean anomaly | 163.9866° |
| Eccentric anomaly | 164.07583° |
| Mean motion | 3.71258 °/min |
| BSTAR | 0.00019244 |
| Orbital period | 96.97 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 |
OV1-10 R/B 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-21 22:49:51.733Z | 168.042° S | 2024-12-21 22:53:51.733Z | 49.392° ENE | 44.507° | 2024-12-21 22:57:51.733Z | 355.694° N |
| 6 mins | 2024-12-22 10:37:51.733Z | 37.381° NE | 2024-12-22 10:40:51.733Z | 100.578° ESE | 26.427° | 2024-12-22 10:43:51.733Z | 150.982° SSE |
| 4 mins | 2024-12-22 12:14:51.733Z | 321.579° NNW | 2024-12-22 12:16:51.733Z | 286.73° WNW | 18.578° | 2024-12-22 12:18:51.733Z | 251.804° W |
Authenticating...
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