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: 1 day ago

TLE from 1 day ago
0 H-2A R/B
1 61440U 24176B   25310.34882285  .00063759  00000-0  10271-2 0  9999
2 61440  97.2603  80.6628 0009599  25.4869 334.6855 15.52688734 62427
Epoch: 2025-11-06T08:22Z
TLE epoch observation values (Epoch: 2025-11-06T08:22:18.294Z)
Latitude
-0.00007°
Longitude
-90.72184°
Altitude
406.129 km
Speed
7.67 km/s
True Right ascension
05h 22m 39s
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
12:11:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
412.308 km
Perigee altitude
399.284 km
Semi-major axis
6,783.933 km
Eccentricity
0.00096
Inclination
97.2603°
RAAN
80.6628°
Arg. of periapsis
25.4869°
True anomaly
334.63842°
Mean anomaly
334.6855°
Eccentric anomaly
334.66196°
Mean motion
3.88437 °/min
Orbital period
92.68 mins
BSTAR
0.0010271
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Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)

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