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: 8 hours ago

TLE from 8 hours ago
0 H-2A R/B
1 43682U 18084L   26083.14192937  .00018225  00000-0  42599-3 0  9999
2 43682  98.8707 303.6244 0024143 335.2715  24.7369 15.41952120408009
Epoch: 2026-03-24T03:24Z
TLE epoch observation values (Epoch: 2026-03-24T03:24:22.697Z)
Latitude
0.00005°
Longitude
70.90599°
Altitude
428.474 km
Speed
7.663 km/s
True Right ascension
20h 14m 29s
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
16:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.809 km
Perigee altitude
420.9 km
Semi-major axis
6,815.491 km
Eccentricity
0.00241
Inclination
98.8707°
RAAN
303.6244°
Arg. of periapsis
335.2715°
True anomaly
24.85299°
Mean anomaly
24.7369°
Eccentric anomaly
24.79491°
Mean motion
3.85742 °/min
Orbital period
93.33 mins
BSTAR
0.00042599
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