H-2A R/B, 61440

Orbit data source: Space-Track

H-2A R/B, 61440 is space debris in SSO originally from a launch on Thu, 26 Sep 2024 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
61440, 2024-176B
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)
2024-09-26 (1 year ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 H-2A R/B
1 61440U 24176B   25295.32455694  .00055578  00000-0  95142-3 0  9990
2 61440  97.2578  65.4908 0010300  83.4688 276.7736 15.51009209 60093
Epoch: 2025-10-22T07:47Z
TLE epoch observation values (Epoch: 2025-10-22T07:47:21.719Z)
Latitude
-0.00009°
Longitude
-82.34948°
Altitude
416.097 km
Speed
7.662 km/s
True Right ascension
04h 21m 57s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
13:53:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.689 km
Perigee altitude
403.704 km
Semi-major axis
6,788.833 km
Eccentricity
0.00103
Inclination
97.2578°
RAAN
65.4908°
Arg. of periapsis
83.4688°
True anomaly
276.65638°
Mean anomaly
276.7736°
Eccentric anomaly
276.71499°
Mean motion
3.88017 °/min
Orbital period
92.78 mins
BSTAR
0.00095142
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Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)

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