H-2A DEB, 43675 (Decayed)
Orbit data source: Space-Track
H-2A DEB, 43675 was space debris in LEO originally from a launch on Mon, 29 Oct 2018 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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43675 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Kawasaki
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 2.0 m
Radar Cross Section
6.654 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 H-2A DEB
1 43675U 18084E 26067.89637679 .14320155 29055-5 13991-2 0 9994
2 43675 97.9890 284.8636 0008171 270.2383 89.7978 16.38301702403004Epoch: 2026-03-08T21:30Z
TLE epoch observation values (Epoch: 2026-03-08T21:30:46.954Z)
Latitude
0.00003°
Longitude
155.57086°
Altitude
173.54 km
Speed
7.802 km/s
True Right ascension
18h 59m 27s
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
16:22:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.51 km
Perigee altitude
161.813 km
Semi-major axis
6,545.298 km
Eccentricity
0.00082
Inclination
97.989°
RAAN
284.8636°
Arg. of periapsis
270.2383°
True anomaly
89.89143°
Mean anomaly
89.7978°
Eccentric anomaly
89.84462°
Mean motion
4.09873 °/min
Orbital period
87.83 mins
BSTAR
0.0013991
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Other satellites on launch #84 in the year 2018 (2018-10-29 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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| 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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