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

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 H-3 R/B
1 62877U 25023B   25242.94272949  .00002332  00000-0  19302-2 0  9990
2 62877  21.0689 220.1679 7213901 324.5815   4.0523  2.33379202  4892
Epoch: 2025-08-30T22:37Z
TLE epoch observation values (Epoch: 2025-08-30T22:37:31.827Z)
Latitude
0.00002°
Longitude
-98.61769°
Altitude
868.119 km
Speed
9.665 km/s
True Right ascension
14h 40m 32s
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
20:42:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,957.109 km
Perigee altitude
312.042 km
Semi-major axis
24,012.712 km
Eccentricity
0.72139
Inclination
21.0689°
RAAN
220.1679°
Arg. of periapsis
324.5815°
True anomaly
34.34039°
Mean anomaly
4.0523°
Eccentric anomaly
14.1717°
Mean motion
0.58329 °/min
Orbital period
617.19 mins
BSTAR
0.0019302
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Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)

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