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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40011 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
AXELSPACE
Mission
Operational Commercial Imaging
Bus & Motor
HODOYOSHI, Unknown motor
Mass
64 kg wet, 64 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HODOYOSHI 4
1 40011U 14033B 26078.93412231 .00001316 00000-0 14892-3 0 9993
2 40011 97.5445 268.0706 0022429 240.0290 119.8701 14.87877772635534Epoch: 2026-03-19T22:25Z
TLE epoch observation values (Epoch: 2026-03-19T22:25:08.167Z)
Latitude
-0.00002°
Longitude
114.31015°
Altitude
615.438 km
Speed
7.547 km/s
True Right ascension
17h 52m 16s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:44:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.237 km
Perigee altitude
585.928 km
Semi-major axis
6,979.719 km
Eccentricity
0.00224
Inclination
97.5445°
RAAN
268.0706°
Arg. of periapsis
240.029°
True anomaly
120.09266°
Mean anomaly
119.8701°
Eccentric anomaly
119.98141°
Mean motion
3.72208 °/min
Orbital period
96.72 mins
BSTAR
0.00014892
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.HODOYOSHI 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-20 11:29:45.256Z | 98.754° ESE | 2026-03-20 11:31:45.256Z | 67.01° ENE | 16.755° | 2026-03-20 11:33:45.256Z | 34.978° NE |
| 6 mins | 2026-03-20 13:04:45.256Z | 202.377° SSW | 2026-03-20 13:07:45.256Z | 278.948° WNW | 32.063° | 2026-03-20 13:10:45.256Z | 329.122° NNW |
| 6 mins | 2026-03-21 00:49:45.256Z | 38.873° NE | 2026-03-21 00:52:45.256Z | 102.321° ESE | 29.243° | 2026-03-21 00:55:45.256Z | 158.266° S |
| 4 mins | 2026-03-21 02:26:45.256Z | 318.328° NNW | 2026-03-21 02:27:45.256Z | 300.726° NW | 18.188° | 2026-03-21 02:30:45.256Z | 251.34° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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