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)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
1.900 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 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 16.38616980478017Epoch: 2024-10-18T20:31Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:28:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.647 km
Perigee altitude
170.441 km
Semi-major axis
6,551.681 km
Eccentricity
0.00047
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
Orbital period
87.96 mins
BSTAR
0.0018819
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Other satellites on launch #12 in the year 2016 (2016-02-17 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ASTRO H DEB Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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