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HIMAWARI 9, 41836

Orbit data source: Space-Track

HIMAWARI 9, 41836 is a payload satellite owned by JMA (JP) in GEO that was launched on Wed, 02 Nov 2016 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days
Identifier
41836, 2016-064A
Orbit
GEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
MELCO
Mission
Operational Civil Weather
Bus & Motor
DS-2000, R-4D
Mass
3,500 kg wet, 1,300 kg dry
Launch date (UTC)
2016-11-02 (9 years ago)
Launch vehicle
H-IIA 202
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan + 1 Rod, 15.0 m
Radar Cross Section
63.551 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 HIMAWARI 9
1 41836U 16064A   25271.88663589  .00000000  00000-0  00000-0 0  9999
2 41836   0.0201 157.4760 0003185  92.6692 217.7126  1.00277571 32593
Epoch: 2025-09-28T21:16Z
TLE epoch observation values (Epoch: 2025-09-28T21:16:45.340Z)
Latitude
-0.03155°
Longitude
140.72506°
Altitude
35,795.046 km
Speed
3.074 km/s
True Right ascension
07h 11m 14s
True Declination
0° 01' 53"
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
12:45:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.473 km
Perigee altitude
35,772.614 km
Semi-major axis
42,164.18 km
Eccentricity
0.00032
Inclination
0.0201°
RAAN
157.476°
Arg. of periapsis
92.6692°
True anomaly
217.69028°
Mean anomaly
217.7126°
Eccentric anomaly
217.70144°
Mean motion
0.25068 °/min
Orbital period
1,436.07 mins
BSTAR
0
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Other satellites on launch #64 in the year 2016 (2016-11-02 UTC)

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