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HIMAWARI 8, 40267

Orbit data source: Space-Track

HIMAWARI 8, 40267 is a payload satellite owned by JMA (JP) in GEO that was launched on Tue, 07 Oct 2014 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
40267, 2014-060A
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)
2014-10-07 (11 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: 6 hours ago

TLE from 6 hours ago
0 HIMAWARI 8
1 40267U 14060A   25342.59474416 -.00000273  00000-0  00000-0 0  9999
2 40267   0.0332 224.0162 0001276  71.8182 136.5361  1.00270585 40848
Epoch: 2025-12-08T14:16Z
TLE epoch observation values (Epoch: 2025-12-08T14:16:25.895Z)
Latitude
0.01134°
Longitude
140.67625°
Altitude
35,790.347 km
Speed
3.074 km/s
True Right ascension
04h 49m 30s
True Declination
0° 00' 41"
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
18:16:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.382 km
Perigee altitude
35,782.621 km
Semi-major axis
42,166.139 km
Eccentricity
0.00013
Inclination
0.0332°
RAAN
224.0162°
Arg. of periapsis
71.8182°
True anomaly
136.54616°
Mean anomaly
136.5361°
Eccentric anomaly
136.54113°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #60 in the year 2014 (2014-10-07 UTC)

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