H-2A R/B, 64695

Orbit data source: Space-Track

H-2A R/B, 64695 is space debris in SSO originally from a launch on Sat, 28 Jun 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
64695, 2025-141B
Orbit
SSO
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)
2025-06-28 (5 months ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 H-2A R/B
1 64695U 25141B   25334.28520708  .00002313  00000-0  22829-3 0  9997
2 64695  98.0636 275.6376 0094294 118.2746 242.8026 14.89719815 23009
Epoch: 2025-11-30T06:50Z
TLE epoch observation values (Epoch: 2025-11-30T06:50:41.891Z)
Latitude
-0.00009°
Longitude
103.56181°
Altitude
632.404 km
Speed
7.526 km/s
True Right ascension
18h 22m 33s
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
21:22:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
661.606 km
Perigee altitude
530.085 km
Semi-major axis
6,973.982 km
Eccentricity
0.00943
Inclination
98.0636°
RAAN
275.6376°
Arg. of periapsis
118.2746°
True anomaly
241.84673°
Mean anomaly
242.8026°
Eccentric anomaly
242.32415°
Mean motion
3.72668 °/min
Orbital period
96.6 mins
BSTAR
0.00022829
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Other satellites on launch #141 in the year 2025 (2025-06-28 UTC)

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