DECAYED

H-2A R/B, 58763 (Decayed)

Orbit data source: Space-Track

H-2A R/B, 58763 was space debris in LEO originally from a launch on Fri, 12 Jan 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.

Not visible in the next 10 days
Identifier
58763, 2024-010B
Orbit
Decayed
Last TLE update
8 months ago
Origin
Manufacturer
MHI Tobishima
Mission
Decayed spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
2024-01-12 (2 years 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

TLE from 8 months ago
0 H-2A R/B
1 58763U 24010B   24338.62726552  .15328433  25498-5  23479-3 0  9991
2 58763  97.1459 102.5365 0007880 230.1601 251.9516 16.48281285 50698
Epoch: 2024-12-03T15:03Z
TLE epoch observation values (Epoch: 2024-12-03T15:03:15.74Z)
Latitude
57.37835°
Longitude
-4.98338°
Altitude
155.193 km
Speed
7.818 km/s
True Right ascension
19h 35m 03s
True Declination
57° 12' 27"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
145.788 km
Perigee altitude
135.514 km
Semi-major axis
6,518.788 km
Eccentricity
0.00079
Inclination
97.1459°
RAAN
102.5365°
Arg. of periapsis
230.1601°
True anomaly
251.86577°
Mean anomaly
251.9516°
Eccentric anomaly
251.90868°
Mean motion
4.12376 °/min
Orbital period
87.3 mins
BSTAR
0.00023479
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