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 (11 months 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: 6 hours ago

TLE from 6 hours ago
0 H-2A R/B
1 61440U 24176B   25243.29186821  .00043736  00000-0  90104-3 0  9998
2 61440  97.2506  13.2761 0011848 272.5541  87.4352 15.45717468 52042
Epoch: 2025-08-31T07:00Z
TLE epoch observation values (Epoch: 2025-08-31T07:00:17.413Z)
Latitude
-0.00002°
Longitude
-71.51036°
Altitude
432.049 km
Speed
7.653 km/s
True Right ascension
00h 53m 06s
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
05:06:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.257 km
Perigee altitude
418.134 km
Semi-major axis
6,804.333 km
Eccentricity
0.00118
Inclination
97.2506°
RAAN
13.2761°
Arg. of periapsis
272.5541°
True anomaly
87.57084°
Mean anomaly
87.4352°
Eccentric anomaly
87.50302°
Mean motion
3.86692 °/min
Orbital period
93.1 mins
BSTAR
0.00090104
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Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)

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