DELTA 1 R/B(1), 10062
Orbit data source: Space-Track
DELTA 1 R/B(1), 10062 is space debris in LEO originally from a launch on Thu, 16 Jun 1977 UTC launched from the Air Force Eastern Test Range (AFETR). 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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10062 intel report (Beta)
DELTA 1 R/B(1) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | MDAC-HB |
| Mission | Spacecraft |
| Bus & Motor | DELTA/TR-201, Unknown motor |
| Mass | 845 kg wet, 845 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl + 1 Nozzle, 6.39 m |
| Radar Cross Section | 7.796 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 5 hours ago
0 DELTA 1 R/B(1)
1 10062U 77048B 24361.79053539 .00000892 00000-0 29129-3 0 9997
2 10062 28.4219 285.0956 0729822 260.1196 91.6262 13.38306046315130Epoch: 2024-12-26T18:58Z
Definitive object data (Epoch: 2024-12-26T18:58:22.257Z)
| Latitude | -0.00002° |
| Longitude | -95.26205° |
| Altitude | 1,169.101 km |
| Speed | 7.244 km/s |
| True Right ascension | 19h 00m 22s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -14.01804° |
| Longitude | -123.67529° |
| Altitude | 876.306 km |
| Speed | 7.534 km/s |
| Apparent Right ascension | 14h 56m 57s |
| Apparent Declination | -32° 42' 17" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 23:35:12 |
| Azimuth | 263.797° W |
| Elevation | -49.267° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,666.708 km |
| Perigee altitude | 572.318 km |
| Semi-major axis | 7,497.65 km |
| Eccentricity | 0.0729822 |
| Inclination | 28.4219° |
| RAAN | 285.0956° |
| Arg. of periapsis | 260.1196° |
| True anomaly | 99.93518° |
| Mean anomaly | 91.6262° |
| Eccentric anomaly | 95.78647° |
| Mean motion | 3.34315 °/min |
| BSTAR | 0.00029129 |
| Orbital period | 107.68 mins |
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Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)
| GOES 2, 10061 |
| DELTA 1 R/B(1), 10062 |
| DELTA 1 DEB, 10063 (Decayed) |
| DELTA 1 DEB, 10067 (Decayed) |
| DELTA 1 DEB, 10075 (Decayed) |
| DELTA 1 R/B(2), 10409 (Decayed) |
| GOES 2 AKM, 20799 |
DELTA 1 R/B(1) 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. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2024-12-27 00:38:45.446Z | 237.724° WSW | 2024-12-27 00:47:45.446Z | 168.502° S | 33.74° | 2024-12-27 00:55:45.446Z | 111.109° ESE |
| 16 mins | 2024-12-27 02:34:45.446Z | 248.979° W | 2024-12-27 02:42:45.446Z | 185.863° SSW | 32.414° | 2024-12-27 02:50:45.446Z | 127.227° SE |
| 12 mins | 2024-12-27 04:30:45.446Z | 248.508° W | 2024-12-27 04:36:45.446Z | 207.553° SW | 21.971° | 2024-12-27 04:42:45.446Z | 161.645° S |
| 13 mins | 2024-12-27 22:01:45.446Z | 197.704° SSW | 2024-12-27 22:07:45.446Z | 150.915° SSE | 23.161° | 2024-12-27 22:14:45.446Z | 106.697° ESE |
| 16 mins | 2024-12-27 23:54:45.446Z | 229.598° WSW | 2024-12-28 00:01:45.446Z | 173.078° S | 32.934° | 2024-12-28 00:10:45.446Z | 108.07° ESE |
Authenticating...
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