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 (1 year 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: 10 hours ago

TLE from 10 hours ago
0 H-2A R/B
1 64695U 25141B   26171.42988034  .00001200  00000-0  11855-3 0  9994
2 64695  98.0864 122.2994 0091021 174.1251 186.1057 14.90957772 53119
Epoch: 2026-06-20T10:19Z
TLE epoch observation values (Epoch: 2026-06-20T10:19:01.661Z)
Latitude
-0.00002°
Longitude
58.89786°
Altitude
661.109 km
Speed
7.493 km/s
True Right ascension
08h 09m 11s
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
07:23:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.425 km
Perigee altitude
528.539 km
Semi-major axis
6,970.119 km
Eccentricity
0.0091
Inclination
98.0864°
RAAN
122.2994°
Arg. of periapsis
174.1251°
True anomaly
185.996°
Mean anomaly
186.1057°
Eccentric anomaly
186.05073°
Mean motion
3.72978 °/min
Orbital period
96.52 mins
BSTAR
0.00011855
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Other satellites on launch #141 in the year 2025 (2025-06-28 UTC)

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