H-2A R/B, 41341

Orbit data source: Space-Track

H-2A R/B, 41341 is space debris in LEO originally from a launch on Wed, 17 Feb 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.

Not visible in the next 10 days
Identifier
41341, 2016-012E
Orbit
LEO
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)
2016-02-17 (10 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: 23 hours ago

TLE from 23 hours ago
0 H-2A R/B
1 41341U 16012E   26123.60804399  .00040186  00000-0  58200-3 0  9993
2 41341  30.6220 220.9517 0006297 131.5878 228.5306 15.54556180564585
Epoch: 2026-05-03T14:35Z
TLE epoch observation values (Epoch: 2026-05-03T14:35:35.000Z)
Latitude
-0.00001°
Longitude
140.5467°
Altitude
404.714 km
Speed
7.669 km/s
True Right ascension
14h 43m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:19:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.689 km
Perigee altitude
403.143 km
Semi-major axis
6,785.553 km
Eccentricity
0.00063
Inclination
30.622°
RAAN
220.9517°
Arg. of periapsis
131.5878°
True anomaly
228.47656°
Mean anomaly
228.5306°
Eccentric anomaly
228.50358°
Mean motion
3.88298 °/min
Orbital period
92.71 mins
BSTAR
0.000582
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