Showing default

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.

Loading next visibility...
Identifier
40015, 2014-033F
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational Amateur Imaging
Bus & Motor
HODOYOSHI, Unknown motor
Mass
58 kg wet, 58 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: 1 day ago

TLE from 1 day ago
0 HODOYOSHI 3
1 40015U 14033F   26302.69952525  .00000674  00000-0  83286-4 0  9995
2 40015  97.6571 100.4917 0031201 271.5317  88.2325 14.85633746667590
Epoch: 2026-10-29T16:47Z
TLE epoch observation values (Epoch: 2026-10-29T16:47:18.981Z)
Latitude
-0°
Longitude
170.63241°
Altitude
614.029 km
Speed
7.552 km/s
True Right ascension
06h 41m 58s
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
13:10:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.419 km
Perigee altitude
586.821 km
Semi-major axis
6,986.757 km
Eccentricity
0.00312
Inclination
97.6571°
RAAN
100.4917°
Arg. of periapsis
271.5317°
True anomaly
88.58991°
Mean anomaly
88.2325°
Eccentric anomaly
88.4112°
Mean motion
3.71646 °/min
Orbital period
96.87 mins
BSTAR
0.000083286
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|