ASTRO H DEB, 41442 (Decayed)
Orbit data source: Space-Track
ASTRO H DEB, 41442 was space debris in LEO originally from a Japanese launch on Wed, 17 Feb 2016 UTC launched from the Tanegashima Space Center (TNSTA). 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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41442 intel report (Beta)
ASTRO H 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 | 1.900 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 ASTRO H DEB
1 41442U 16012L 24292.85535606 .22936264 -40466-5 18819-2 0 9991
2 41442 30.9758 142.5786 0004736 277.6116 190.0773 16.38616980478017
Epoch: 2024-10-18T20:31Z
Definitive object data (Epoch: 2024-10-18T20:31:42.763Z)
Latitude | 29.50344° |
Longitude | -82.7574° |
Altitude | 171.645 km |
Speed | 7.807 km/s |
True Right ascension | 16h 51m 57s |
True Declination | 29° 20' 35" |
Sunlit | Object was in daylight 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 | 176.647 km |
Perigee altitude | 170.441 km |
Semi-major axis | 6,551.681 km |
Eccentricity | 0.0004736 |
Inclination | 30.9758° |
RAAN | 142.5786° |
Arg. of periapsis | 277.6116° |
True anomaly | 190.06781° |
Mean anomaly | 190.0773° |
Eccentric anomaly | 190.07255° |
Mean motion | 4.09274 °/min |
BSTAR | 0.0018819 |
Orbital period | 87.96 mins |
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Other satellites on launch #12 in the year 2016 (2016-02-17 UTC)
ASTRO H DEB Visibility forecast
Observer location: undefined°, undefined
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