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HODOYOSHI 3, 40015

Orbit data source: Space-Track

HODOYOSHI 3, 40015 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
40015, 2014-033F
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational Commercial Imaging
Bus & Motor
HODOYOSHI, Unknown motor
Mass
58 kg wet, 58 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: 10 hours ago

TLE from 10 hours ago
0 HODOYOSHI 3
1 40015U 14033F   25288.72843837  .00002517  00000-0  30170-3 0  9997
2 40015  97.6192  97.1046 0034741  80.1457 280.3678 14.84499476611342
Epoch: 2025-10-15T17:28Z
TLE epoch observation values (Epoch: 2025-10-15T17:28:57.075Z)
Latitude
0.00003°
Longitude
170.36844°
Altitude
613.902 km
Speed
7.554 km/s
True Right ascension
06h 28m 25s
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
22:02:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.465 km
Perigee altitude
587.895 km
Semi-major axis
6,990.317 km
Eccentricity
0.00347
Inclination
97.6192°
RAAN
97.1046°
Arg. of periapsis
80.1457°
True anomaly
279.97589°
Mean anomaly
280.3678°
Eccentric anomaly
280.17188°
Mean motion
3.71362 °/min
Orbital period
96.94 mins
BSTAR
0.0003017
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