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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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<iframe src="https://www.satcat.com/sats-embedded/40015?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/40015?theme=dark&initialShowStats=false

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Identifier

40015, 2014-033F

Orbit

SSO

Country

JP / JPN

Related business

The University of Tokyo (JP)

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: 9 hours ago

TLE from 9 hours ago

0 HODOYOSHI 3
1 40015U 14033F   25334.69417353  .00001897  00000-0  22807-3 0  9993
2 40015  97.6195 141.0533 0031936 289.2295  70.5466 14.84738464618164

Epoch: 2025-11-30T16:39Z

TLE epoch observation values (Epoch: 2025-11-30T16:39:36.592Z)

Latitude

0.00002°

Longitude

-178.65353°

Altitude

610.068 km

Speed

7.558 km/s

True Right ascension

09h 24m 12s

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

23:25:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

633.751 km

Perigee altitude

589.107 km

Semi-major axis

6,989.566 km

Eccentricity

0.00319

Inclination

97.6195°

RAAN

141.0533°

Arg. of periapsis

289.2295°

True anomaly

70.89213°

Mean anomaly

70.5466°

Eccentric anomaly

70.71932°

Mean motion

3.71422 °/min

Orbital period

96.92 mins

BSTAR

0.00022807

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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)

FLOCK 1C 10, 40023 (Decayed)

FLOCK 1C 2, 40029 (Decayed)

FLOCK 1C 9, 40035 (Decayed)

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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.

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HODOYOSHI 3 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.
6 mins	2025-12-01 10:35:40.184Z	125.177° SE	2025-12-01 10:38:40.184Z	67.441° ENE	27.197°	2025-12-01 10:41:40.184Z	13.945° NNE
5 mins	2025-12-01 12:12:40.184Z	230.969° WSW	2025-12-01 12:14:40.184Z	267.449° W	20.302°	2025-12-01 12:17:40.184Z	314.308° NW
7 mins	2025-12-01 23:58:40.184Z	21.07° NNE	2025-12-02 00:01:40.184Z	133.762° SE	42.683°	2025-12-02 00:05:40.184Z	185.654° SSW

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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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Check out HODOYOSHI 3, 40015 on other resources

View HODOYOSHI 3, 40015 on NASA - NSSDCA Website

View HODOYOSHI 3, 40015 on Heavens-Above

View HODOYOSHI 3, 40015 on Keep Track

View HODOYOSHI 3, 40015 on Celestrak

View HODOYOSHI 3, 40015 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

HODOYOSHI 3, 40015

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2025-11-30T16:39:36.592Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)

HODOYOSHI 3 Visibility forecast

Co-orbital & Co-planar RSOs

Check out HODOYOSHI 3, 40015 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago