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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: 7 hours ago

TLE from 7 hours ago
0 HODOYOSHI 4
1 40011U 14033B   25343.58170307  .00001757  00000-0  19880-3 0  9994
2 40011  97.5412 172.6212 0023014 211.4456 148.5387 14.87462213620619
Epoch: 2025-12-09T13:57Z
TLE epoch observation values (Epoch: 2025-12-09T13:57:39.145Z)
Latitude
0.00003°
Longitude
-115.35623°
Altitude
622.633 km
Speed
7.54 km/s
True Right ascension
11h 30m 29s
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
19:13:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
618.949 km
Perigee altitude
586.817 km
Semi-major axis
6,981.02 km
Eccentricity
0.0023
Inclination
97.5412°
RAAN
172.6212°
Arg. of periapsis
211.4456°
True anomaly
148.676°
Mean anomaly
148.5387°
Eccentric anomaly
148.60739°
Mean motion
3.72104 °/min
Orbital period
96.75 mins
BSTAR
0.0001988
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