DELTA 1 DEB (YO), 312
Orbit data source: Space-Track
DELTA 1 DEB (YO), 312 is space debris in LEO originally from a launch on Tue, 19 Jun 1962 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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312 intel report (Beta)
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Edit Public Description
Identifier | |
Orbit | LEO |
Last TLE update | 21 hours ago |
Origin | |
Manufacturer | RCA/East Windsor |
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 | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 DELTA 1 DEB (YO)
1 00312U 62025C 25074.91150056 .00004129 00000-0 67746-3 0 9995
2 00312 58.2443 263.3855 0199437 53.9764 307.9568 14.60144439291942
Epoch: 2025-03-15T21:52Z
Definitive object data (Epoch: 2025-03-15T21:52:33.648Z)
Latitude | -0.00004° |
Longitude | 121.49503° |
Altitude | 609.134 km |
Speed | 7.601 km/s |
True Right ascension | 17h 33m 32s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 3.29665° |
Longitude | -63.66193° |
Altitude | 764.091 km |
Speed | 7.436 km/s |
Apparent Right ascension | 07h 26m 54s |
Apparent Declination | -22° 27' 11" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 23:00:44 |
Azimuth | 85.367° E |
Elevation | -41.846° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 833.194 km |
Perigee altitude | 551.177 km |
Semi-major axis | 7,070.322 km |
Eccentricity | 0.0199437 |
Inclination | 58.2443° |
RAAN | 263.3855° |
Arg. of periapsis | 53.9764° |
True anomaly | 306.1271° |
Mean anomaly | 307.9568° |
Eccentric anomaly | 307.04474° |
Mean motion | 3.65077 °/min |
BSTAR | 0.00067746 |
Orbital period | 98.61 mins |
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)
TIROS 5, 309 |
DELTA 1 R/B, 311 (Decayed) |
DELTA 1 DEB (YO), 313 (Decayed) |
DELTA 1 DEB, 6251 (Decayed) |
DELTA 1 DEB (YO) 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. |
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7 mins | 2025-03-16 21:21:50.766Z | 344.359° N | 2025-03-16 21:24:50.766Z | 34.675° NE | 24.17° | 2025-03-16 21:28:50.766Z | 94.854° ESE |
7 mins | 2025-03-16 23:04:50.766Z | 295.754° NW | 2025-03-16 23:06:50.766Z | 252.645° W | 35.857° | 2025-03-16 23:11:50.766Z | 160.569° S |
5 mins | 2025-03-17 13:27:50.766Z | 160.344° S | 2025-03-17 13:29:50.766Z | 123.005° SE | 20.604° | 2025-03-17 13:32:50.766Z | 72.402° E |
5 mins | 2025-03-17 15:09:50.766Z | 263.912° W | 2025-03-17 15:11:50.766Z | 318.998° NNW | 32.218° | 2025-03-17 15:14:50.766Z | 23.215° NE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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