DELTA 1 DEB (YO), 167
Orbit data source: Space-Track
DELTA 1 DEB (YO), 167 is space debris in LEO originally from a launch on Wed, 12 Jul 1961 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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167 intel report (Beta)
DELTA 1 DEB (YO) details
Identifier | |
Orbit | LEO |
Last TLE update | 1 day 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 1 day ago
0 DELTA 1 DEB (YO)
1 00167U 61017D 25001.51413843 .00001126 00000-0 53271-3 0 9997
2 00167 47.8438 226.3298 0090569 93.3905 267.7343 14.23763370288905
Epoch: 2025-01-01T12:20Z
Definitive object data (Epoch: 2025-01-01T12:20:21.56Z)
Latitude | -0.00005° |
Longitude | -60.16641° |
Altitude | 816.118 km |
Speed | 7.445 km/s |
True Right ascension | 15h 05m 19s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 43.79778° |
Longitude | 54.47285° |
Altitude | 752.984 km |
Speed | 7.517 km/s |
Apparent Right ascension | 02h 41m 12s |
Apparent Declination | 10° 07' 59" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 19:00:32 |
Azimuth | 65.631° ENE |
Elevation | -12.017° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 878.87 km |
Perigee altitude | 748.598 km |
Semi-major axis | 7,191.871 km |
Eccentricity | 0.0090569 |
Inclination | 47.8438° |
RAAN | 226.3298° |
Arg. of periapsis | 93.3905° |
True anomaly | 266.69779° |
Mean anomaly | 267.7343° |
Eccentric anomaly | 267.21599° |
Mean motion | 3.55861 °/min |
BSTAR | 0.00053271 |
Orbital period | 101.16 mins |
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Other satellites on launch #17 in the year 1961 (1961-07-12 UTC)
TIROS 3, 162 |
DELTA 1 R/B, 165 (Decayed) |
DELTA 1 DEB (YO), 166 (Decayed) |
DELTA 1 DEB (YO), 167 |
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. |
---|---|---|---|---|---|---|---|
8 mins | 2025-01-02 20:41:19.105Z | 298.713° NW | 2025-01-02 20:45:19.105Z | 2.634° NNE | 29.452° | 2025-01-02 20:49:19.105Z | 60.984° ENE |
8 mins | 2025-01-02 22:28:19.105Z | 309.801° NW | 2025-01-02 22:32:19.105Z | 35.751° NE | 37.252° | 2025-01-02 22:36:19.105Z | 93.465° ESE |
8 mins | 2025-01-03 00:14:19.105Z | 286.945° WNW | 2025-01-03 00:18:19.105Z | 203.017° SW | 37.31° | 2025-01-03 00:22:19.105Z | 145.878° SSE |
8 mins | 2025-01-03 16:43:19.105Z | 202.991° SW | 2025-01-03 16:47:19.105Z | 135.848° SSE | 33.297° | 2025-01-03 16:51:19.105Z | 74.631° E |
8 mins | 2025-01-03 18:29:19.105Z | 262.362° W | 2025-01-03 18:33:19.105Z | 349.275° N | 40.152° | 2025-01-03 18:37:19.105Z | 54.051° ENE |
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