H-2A R/B, 43682

Orbit data source: Space-Track

H-2A R/B, 43682 is space debris in SSO 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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Identifier
43682, 2018-084L
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
MHI Tobishima
Mission
Spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
2018-10-29 (7 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 H-2A R/B
1 43682U 18084L   26034.11343896  .00020199  00000-0  50558-3 0  9991
2 43682  98.8754 244.1514 0026276 141.8922 218.4184 15.39797196400455
Epoch: 2026-02-03T02:43Z
TLE epoch observation values (Epoch: 2026-02-03T02:43:21.126Z)
Latitude
-0°
Longitude
70.01434°
Altitude
463.851 km
Speed
7.627 km/s
True Right ascension
16h 16m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:36:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.643 km
Perigee altitude
425.792 km
Semi-major axis
6,821.855 km
Eccentricity
0.00263
Inclination
98.8754°
RAAN
244.1514°
Arg. of periapsis
141.8922°
True anomaly
218.23178°
Mean anomaly
218.4184°
Eccentric anomaly
218.32504°
Mean motion
3.85203 °/min
Orbital period
93.46 mins
BSTAR
0.00050558
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