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HODOYOSHI 4, 40011

Orbit data source: Space-Track

HODOYOSHI 4, 40011 is a payload satellite owned by Tokyo (JP) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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.

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Identifier
40011, 2014-033B
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational Commercial Imaging
Bus & Motor
HODOYOSHI, Unknown motor
Mass
64 kg wet, 64 kg dry
Launch date (UTC)
2014-06-19 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.614 m², Medium (>0.1 m² and < 1m²)

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

TLE from 22 hours ago
0 HODOYOSHI 4
1 40011U 14033B   26172.53914405  .00001346  00000-0  15121-3 0  9993
2 40011  97.5457 357.1508 0022176 293.0169  66.8709 14.88136903649459
Epoch: 2026-06-21T12:56Z
TLE epoch observation values (Epoch: 2026-06-21T12:56:22.045Z)
Latitude
-0.0001°
Longitude
-106.67901°
Altitude
600.746 km
Speed
7.563 km/s
True Right ascension
23h 48m 36s
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
21:47:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.248 km
Perigee altitude
585.295 km
Semi-major axis
6,978.908 km
Eccentricity
0.00222
Inclination
97.5457°
RAAN
357.1508°
Arg. of periapsis
293.0169°
True anomaly
67.10485°
Mean anomaly
66.8709°
Eccentric anomaly
66.98785°
Mean motion
3.72273 °/min
Orbital period
96.7 mins
BSTAR
0.00015121
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