H-3 R/B, 62877

Orbit data source: Space-Track

H-3 R/B, 62877 is space debris in HEO originally from a launch on Sun, 02 Feb 2025 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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H-3 R/B details

Identifier	62877, 2025-023B
Orbit	HEO
Last TLE update	3 days ago
Origin	MHI (JP / JPN)
Manufacturer	MHI Tobishima
Mission	Spacecraft
Bus & Motor	H-2A STAGE 2, Unknown motor
Mass	2,500 kg wet, 2,500 kg dry
Launch date (UTC)	2025-02-02 (2 weeks ago)
Launch vehicle	Unknown
Launch site	Tanegashima Space Center (TNSTA)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	RCS unknown

Expand to show TLE details & history

TLE from 3 days ago

0 H-3 R/B
1 62877U 25023B   25044.78701506  .00010102  00000-0  26172-2 0  9995
2 62877  21.3938 299.4308 7251931 183.3744 165.4572  2.31964118   253

Epoch: 2025-02-13T18:53Z

Definitive object data (Epoch: 2025-02-13T18:53:18.101Z)

Latitude	0.00001°
Longitude	-127.93578°
Altitude	35,034.835 km
Speed	1.648 km/s
True Right ascension	19h 57m 47s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	6.43167°
Longitude	-112.25712°
Altitude	32,718.467 km
Speed	1.963 km/s
Apparent Right ascension	21h 26m 22s
Apparent Declination	0° 25' 36"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	13:39:29
Azimuth	71.767° E
Elevation	-19.883°
Doppler factor	1

Orbital elements

Apogee altitude	35,216.754 km
Perigee altitude	247.535 km
Semi-major axis	24,110.281 km
Eccentricity	0.7251931
Inclination	21.3938°
RAAN	299.4308°
Arg. of periapsis	183.3744°
True anomaly	176.62536°
Mean anomaly	165.4572°
Eccentric anomaly	171.55751°
Mean motion	0.57975 °/min
BSTAR	0.0026172
Orbital period	620.96 mins