HIMAWARI 1 AKM, 59985

Orbit data source: Space-Track

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.

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Identifier
59985, 1977-065GQ
Orbit
GEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 27, Unknown motor
Mass
Wet unknown, 24 kg dry
Launch date (UTC)
1977-07-14 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
SPHERE + CONE, 8.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 HIMAWARI 1 AKM
1 59985U 77065GQ  26269.88331447 -.00000273  00000-0  00000+0 0  9996
2 59985   3.9476 271.8747 0275199 126.7194 235.4617  1.01121300 47475
Epoch: 2026-09-26T21:11Z
TLE epoch observation values (Epoch: 2026-09-26T21:11:58.370Z)
Latitude
-0°
Longitude
-52.20096°
Altitude
36,221.525 km
Speed
3.034 km/s
True Right ascension
18h 05m 54s
True Declination
0° 00' 00"
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
03:38:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,705.074 km
Perigee altitude
34,397.293 km
Semi-major axis
41,929.321 km
Eccentricity
0.02752
Inclination
3.9476°
RAAN
271.8747°
Arg. of periapsis
126.7194°
True anomaly
232.91454°
Mean anomaly
235.4617°
Eccentric anomaly
234.18311°
Mean motion
0.25279 °/min
Orbital period
1,424.09 mins
BSTAR
0
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