H-2A R/B, 41837

Orbit data source: Space-Track

H-2A R/B, 41837 is space debris in HEO originally from a launch on Wed, 02 Nov 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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Identifier
41837, 2016-064B
Orbit
HEO
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)
2016-11-02 (9 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: 18 hours ago

TLE from 18 hours ago
0 H-2A R/B
1 41837U 16064B   26016.34800114  .00009357  00000-0  73390-3 0  9995
2 41837  22.5969 324.1762 6388366 209.1082  91.3116  3.51278862 92605
Epoch: 2026-01-16T08:21Z
TLE epoch observation values (Epoch: 2026-01-16T08:21:07.298Z)
Latitude
0.00009°
Longitude
83.12216°
Altitude
18,134.686 km
Speed
3.274 km/s
True Right ascension
21h 36m 45s
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
03:19:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,585.943 km
Perigee altitude
225.285 km
Semi-major axis
18,283.751 km
Eccentricity
0.63884
Inclination
22.5969°
RAAN
324.1762°
Arg. of periapsis
209.1082°
True anomaly
150.9793°
Mean anomaly
91.3116°
Eccentric anomaly
122.26303°
Mean motion
0.8779 °/min
Orbital period
410.07 mins
BSTAR
0.0007339
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Other satellites on launch #64 in the year 2016 (2016-11-02 UTC)

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