HIMAWARI 5 AKM, 23524

Orbit data source: Space-Track

HIMAWARI 5 AKM, 23524 is space debris in GEO originally from a launch on Sat, 18 Mar 1995 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
23524, 1995-011D
Orbit
GEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 27, Unknown motor
Mass
Wet unknown, ~62 kg dry
Launch date (UTC)
1995-03-18 (31 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.7 m
Radar Cross Section
0.907 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 HIMAWARI 5 AKM
1 23524U 95011D   25348.47168123 -.00000350  00000-0  00000-0 0  9995
2 23524  13.6842 349.5971 0217196   9.3395 172.7768  1.01258580 45215
Epoch: 2025-12-14T11:19Z
TLE epoch observation values (Epoch: 2025-12-14T11:19:13.258Z)
Latitude
-0.58011°
Longitude
-81.23655°
Altitude
36,410.734 km
Speed
3.019 km/s
True Right ascension
11h 27m 48s
True Declination
0° 34' 46"
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
13:22:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,423.062 km
Perigee altitude
34,603.336 km
Semi-major axis
41,891.336 km
Eccentricity
0.02172
Inclination
13.6842°
RAAN
349.5971°
Arg. of periapsis
9.3395°
True anomaly
173.08152°
Mean anomaly
172.7768°
Eccentric anomaly
172.92997°
Mean motion
0.25314 °/min
Orbital period
1,422.15 mins
BSTAR
0
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