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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: 4 hours ago

TLE from 4 hours ago
0 HODOYOSHI 4
1 40011U 14033B   26033.53698190  .00001543  00000-0  17416-3 0  9997
2 40011  97.5421 224.8776 0024613  34.5735 325.7077 14.87709370628783
Epoch: 2026-02-02T12:53Z
TLE epoch observation values (Epoch: 2026-02-02T12:53:15.236Z)
Latitude
0.00002°
Longitude
-101.16674°
Altitude
593.947 km
Speed
7.571 km/s
True Right ascension
14h 59m 30s
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
19:12:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.29 km
Perigee altitude
584.929 km
Semi-major axis
6,980.246 km
Eccentricity
0.00246
Inclination
97.5421°
RAAN
224.8776°
Arg. of periapsis
34.5735°
True anomaly
325.54839°
Mean anomaly
325.7077°
Eccentric anomaly
325.62808°
Mean motion
3.72166 °/min
Orbital period
96.73 mins
BSTAR
0.00017416
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