Satellite description

HIMAWARI 1 AKM, 59985 is space debris in GEO originally from a launch on Thu, 14 Jul 1977 UTC launched from the Air Force Eastern Test Range (AFETR). 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.

Satellite metadata
Identifier
59985, 1977-065GQ
Orbit
GEO
Last TLE update
16 hours ago
Origin
Flag of undefinedNASDA (JP)
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 27, Unknown motor
Mass
Wet unknown, 24 kg dry
Launch date (UTC)
1977-07-14 (48 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Visualization orbit readout
Latitude
-4.89699°
Longitude
154.24456°
Altitude
36,414.39 km
Speed
3.02 km/s
Apparent Right ascension
11h 25m 30s
Apparent Declination
-11° 29' 55"
Sunlit
Object is in daylight
Orbital elements
Apogee altitude
36,696.454 km
Perigee altitude
34,403.457 km
Semi-major axis
41,928.093 km
Eccentricity
0.02734
Inclination
5.1759°
RAAN
278.802°
Arg. of periapsis
110.3697°
True anomaly
Unknown
Mean anomaly
252.7307°
Eccentric anomaly
Unknown
Mean motion
0.2528 °/min
Orbital period
1,424.02 mins
BSTAR
0
59985, HIMAWARI 1 AKM
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