SL-16 DEB, 42250 (Decayed)
Orbit data source: Space-Track
SL-16 DEB, 42250 was space debris in LEO originally from a launch on Fri, 26 Mar 1993 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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42250 intel report (Beta)
SL-16 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 2 months ago |
Origin | |
Manufacturer | Unknown |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
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 2 months ago
0 SL-16 DEB
1 42250U 93016DE 24315.10376266 .16752230 00000-0 90591-1 0 9999
2 42250 70.9283 90.2544 0027389 344.1828 15.8518 15.75539387469085
Epoch: 2024-11-10T02:29Z
Definitive object data (Epoch: 2024-11-10T02:29:25.093Z)
Latitude | -0.0001° |
Longitude | 3.15163° |
Altitude | 327.962 km |
Speed | 7.722 km/s |
True Right ascension | 06h 01m 01s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 359.277 km |
Perigee altitude | 322.472 km |
Semi-major axis | 6,719.011 km |
Eccentricity | 0.0027389 |
Inclination | 70.9283° |
RAAN | 90.2544° |
Arg. of periapsis | 344.1828° |
True anomaly | 15.93781° |
Mean anomaly | 15.8518° |
Eccentric anomaly | 15.89478° |
Mean motion | 3.94081 °/min |
BSTAR | 0.090591 |
Orbital period | 91.35 mins |
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Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)
SL-16 DEB 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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