DELTA 1 DEB, 1312
Orbit data source: Space-Track
DELTA 1 DEB, 1312 is space debris in LEO originally from a launch on Fri, 22 Jan 1965 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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1312 intel report (Beta)
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DELTA 1 DEB details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | Unknown |
| Mission | Spacecraft |
| Bus & Motor | Unknown |
| Mass | ~1 kg wet, ~1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Cable, 3.5 m |
| Radar Cross Section | 6.125 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 DELTA 1 DEB
1 01312U 65004C 24295.43902348 .00000912 00000-0 93029-3 0 9995
2 01312 96.3493 208.1791 1118156 22.5697 342.0830 12.27959975652475Epoch: 2024-10-21T10:32Z
Definitive object data (Epoch: 2024-10-21T10:32:11.628Z)
| Latitude | 0.00004° |
| Longitude | 19.76497° |
| Altitude | 727.401 km |
| Speed | 7.875 km/s |
| True Right ascension | 13h 52m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 9.25692° |
| Longitude | -158.4969° |
| Altitude | 2,310.942 km |
| Speed | 6.446 km/s |
| Apparent Right ascension | 01h 55m 17s |
| Apparent Declination | -11° 15' 05" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 13:47:36 |
| Azimuth | 356.08° N |
| Elevation | -61.285° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 2,442.427 km |
| Perigee | 668.254 km |
| Semi-major axis | 7,933.477 km |
| Eccentricity | 0.1118156 |
| Inclination | 96.3493° |
| RAAN | 208.1791° |
| Arg. of periapsis | 22.5697° |
| True anomaly | 337.54576° |
| Mean anomaly | 342.083° |
| Eccentric anomaly | 339.87913° |
| Mean motion | 3.07148 °/min |
| BSTAR | 0.00093029 |
| Period | 117.21 mins |
No data available
No data available
Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)
| TIROS 9, 978 |
| DELTA 1 R/B, 979 |
| DELTA 1 DEB, 1312 |
| DELTA 1 DEB, 1313 |
| DELTA 1 DEB, 27720 |
DELTA 1 DEB Visibility forecast
Observer location: 39.9160978°, -105.1181434
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 | 2024-10-23 06:06:20.177Z | 25.691° NE | 2024-10-23 06:14:20.177Z | 95.146° ESE | 37.387° | 2024-10-23 06:26:20.177Z | 168.689° S |
| 18 mins | 2024-10-23 08:03:20.177Z | 351.461° N | 2024-10-23 08:10:20.177Z | 284.486° WNW | 36.195° | 2024-10-23 08:21:20.177Z | 221.426° SW |
| 6 mins | 2024-10-23 17:26:20.177Z | 103.51° ESE | 2024-10-23 17:28:20.177Z | 67.269° ENE | 22.728° | 2024-10-23 17:32:20.177Z | 14.062° NNE |