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.

Not visible in the next 10 days
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
Unknown shape, 8.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 1 day ago
0 HIMAWARI 1 AKM
1 59985U 77065GQ  26087.93699893 -.00000429  00000-0  00000+0 0  9995
2 59985   4.4064 274.5196 0277360 119.9794 242.4778  1.01123097 45631
Epoch: 2026-03-28T22:29Z
TLE epoch observation values (Epoch: 2026-03-28T22:29:16.707Z)
Latitude
-0.00001°
Longitude
110.55144°
Altitude
36,107.122 km
Speed
3.043 km/s
True Right ascension
18h 16m 53s
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
12:21:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,713.623 km
Perigee altitude
34,387.747 km
Semi-major axis
41,928.822 km
Eccentricity
0.02774
Inclination
4.4064°
RAAN
274.5196°
Arg. of periapsis
119.9794°
True anomaly
239.70472°
Mean anomaly
242.4778°
Eccentric anomaly
241.08673°
Mean motion
0.2528 °/min
Orbital period
1,424.06 mins
BSTAR
0
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