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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 (11 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: 4 hours ago

TLE from 4 hours ago
0 HODOYOSHI 4
1 40011U 14033B   25288.95312352  .00002651  00000-0  29883-3 0  9999
2 40011  97.5464 120.6849 0024936  37.8066 322.4896 14.87184436612499
Epoch: 2025-10-15T22:52Z
TLE epoch observation values (Epoch: 2025-10-15T22:52:29.872Z)
Latitude
-0.00005°
Longitude
112.84063°
Altitude
595.976 km
Speed
7.569 km/s
True Right ascension
08h 02m 44s
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
21:58:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.163 km
Perigee altitude
586.343 km
Semi-major axis
6,981.89 km
Eccentricity
0.00249
Inclination
97.5464°
RAAN
120.6849°
Arg. of periapsis
37.8066°
True anomaly
322.31518°
Mean anomaly
322.4896°
Eccentric anomaly
322.40243°
Mean motion
3.72035 °/min
Orbital period
96.77 mins
BSTAR
0.00029883
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