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 (8 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: 8 hours ago

TLE from 8 hours ago
0 H-2A R/B
1 64695U 25141B   26061.81890210  .00002516  00000-0  24453-3 0  9992
2 64695  98.0758  10.1038 0091825 174.1250 186.1067 14.90427936 36785
Epoch: 2026-03-02T19:39Z
TLE epoch observation values (Epoch: 2026-03-02T19:39:13.141Z)
Latitude
-0.00007°
Longitude
-85.30779°
Altitude
663.333 km
Speed
7.491 km/s
True Right ascension
00h 40m 24s
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
07:13:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
657.653 km
Perigee altitude
529.617 km
Semi-major axis
6,971.772 km
Eccentricity
0.00918
Inclination
98.0758°
RAAN
10.1038°
Arg. of periapsis
174.125°
True anomaly
185.99603°
Mean anomaly
186.1067°
Eccentric anomaly
186.05124°
Mean motion
3.72845 °/min
Orbital period
96.55 mins
BSTAR
0.00024453
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Other satellites on launch #141 in the year 2025 (2025-06-28 UTC)

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