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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Identifier
62877, 2025-023B
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
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 (7 months ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.5 m
Radar Cross Section
55.543 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 H-3 R/B
1 62877U 25023B   25260.07719184  .00002878  00000-0  25052-2 0  9995
2 62877  21.0550 213.3851 7212723 336.7733   2.5146  2.33470273  5299
Epoch: 2025-09-17T01:51Z
TLE epoch observation values (Epoch: 2025-09-17T01:51:09.374Z)
Latitude
0.00001°
Longitude
-170.7238°
Altitude
535.869 km
Speed
9.934 km/s
True Right ascension
14h 13m 17s
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
15:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,943.533 km
Perigee altitude
313.131 km
Semi-major axis
24,006.469 km
Eccentricity
0.72127
Inclination
21.055°
RAAN
213.3851°
Arg. of periapsis
336.7733°
True anomaly
21.95949°
Mean anomaly
2.5146°
Eccentric anomaly
8.92832°
Mean motion
0.58351 °/min
Orbital period
616.95 mins
BSTAR
0.0025052
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Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)

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