H-2A DEB, 43068
Orbit data source: Space-Track
H-2A DEB, 43068 is space debris in SSO originally from a launch on Sat, 23 Dec 2017 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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43068 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 H-2A DEB
1 43068U 17082D 25361.43062058 .00596176 14426-3 17482-2 0 9992
2 43068 97.9934 166.0336 0019825 153.2960 206.9338 15.92376814437001Epoch: 2025-12-27T10:20Z
TLE epoch observation values (Epoch: 2025-12-27T10:20:05.618Z)
Latitude
0.00002°
Longitude
-85.14687°
Altitude
310.607 km
Speed
7.715 km/s
True Right ascension
11h 04m 08s
True Declination
0° 00' 00"
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
08:34:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
305.755 km
Perigee altitude
279.306 km
Semi-major axis
6,670.668 km
Eccentricity
0.00198
Inclination
97.9934°
RAAN
166.0336°
Arg. of periapsis
153.296°
True anomaly
206.83112°
Mean anomaly
206.9338°
Eccentric anomaly
206.88244°
Mean motion
3.98372 °/min
Orbital period
90.37 mins
BSTAR
0.0017482
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Other satellites on launch #82 in the year 2017 (2017-12-23 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.H-2A 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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| H-2A DEB is likely not visible in the next few days. |
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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