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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
Last TLE update
13 hours ago
Origin
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, 30 m
Radar Cross Section
63.551 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 13 hours ago
0 HIMAWARI 9
1 41836U 16064A   25167.74694730 -.00000264  00000-0  00000-0 0  9993
2 41836   0.0522 106.6482 0001419   8.6384 199.6313  1.00269668 31547
Epoch: 2025-06-16T17:55Z
TLE epoch observation values (Epoch: 2025-06-16T17:55:36.246Z)
Latitude
-0.03705°
Longitude
140.75474°
Altitude
35,792.326 km
Speed
3.074 km/s
True Right ascension
20h 59m 38s
True Declination
0° 02' 13"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.04083°
Longitude
-31.0756°
Altitude
35,781.431 km
Speed
3.075 km/s
Apparent Right ascension
09h 09m 11s
Apparent Declination
-5° 12' 06"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
17:08:47
Azimuth
286.088° WNW
Elevation
-26.035°
Doppler factor
1
Orbital elements
Apogee altitude
35,794.242 km
Perigee altitude
35,782.275 km
Semi-major axis
42,166.396 km
Eccentricity
0.00014
Inclination
0.0522°
RAAN
106.6482°
Arg. of periapsis
8.6384°
True anomaly
Unknown
Mean anomaly
199.6313°
Eccentric anomaly
Unknown
Mean motion
0.25066 °/min
Orbital period
1,436.18 mins
BSTAR
0
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41836 neighbors
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Other satellites on launch #64 in the year 2016 (2016-11-02 UTC)

HIMAWARI 9 Visibility

Observer location: undefined°, undefined°

HIMAWARI 9 is likely not visible in the next few days
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