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

H-2A R/B details

Identifier	41341, 2016-012E
Orbit	LEO
Last TLE update	8 hours ago
Origin	MHI (JP / JPN)
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 (9 years ago)
Launch vehicle	Unknown
Launch site	Tanegashima Space Center (TNSTA)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 9.2 m
Radar Cross Section	35.186 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 8 hours ago

0 H-2A R/B
1 41341U 16012E   24361.20107578  .00024603  00000-0  88456-3 0  9998
2 41341  30.6218 324.8906 0011320 281.2550  78.6813 15.27349513488482

Epoch: 2024-12-26T04:49Z

Definitive object data (Epoch: 2024-12-26T04:49:32.947Z)

Latitude	-0.00004°
Longitude	157.31938°
Altitude	480.685 km
Speed	7.629 km/s
True Right ascension	21h 39m 33s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	30.44435°
Longitude	-124.03474°
Altitude	490.185 km
Speed	7.621 km/s
Apparent Right ascension	01h 46m 04s
Apparent Declination	-3° 24' 14"
Sunlit	Object is in full shadow

Visualization observer readout

Local Sidereal Time	12:23:09
Azimuth	327.444° NNW
Elevation	-48.951°
Doppler factor	1

Orbital elements

Apogee altitude	495.438 km
Perigee altitude	479.894 km
Semi-major axis	6,865.803 km
Eccentricity	0.001132
Inclination	30.6218°
RAAN	324.8906°
Arg. of periapsis	281.255°
True anomaly	78.80853°
Mean anomaly	78.6813°
Eccentric anomaly	78.74491°
Mean motion	3.8151 °/min
BSTAR	0.00088456
Orbital period	94.36 mins