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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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ISO8601 Format

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: 10 hours ago

TLE from 10 hours ago

0 HODOYOSHI 3
1 40015U 14033F   25342.44429928  .00002935  00000-0  34897-3 0  9992
2 40015  97.6198 148.4663 0031820 262.7037  97.0561 14.84784577619318

Epoch: 2025-12-08T10:39Z

TLE epoch observation values (Epoch: 2025-12-08T10:39:47.457Z)

Latitude

-0.00006°

Longitude

-88.92467°

Altitude

620.102 km

Speed

7.547 km/s

True Right ascension

09h 53m 51s

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

18:35:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

633.525 km

Perigee altitude

589.044 km

Semi-major axis

6,989.421 km

Eccentricity

0.00318

Inclination

97.6198°

RAAN

148.4663°

Arg. of periapsis

262.7037°

True anomaly

97.41779°

Mean anomaly

97.0561°

Eccentric anomaly

97.23696°

Mean motion

3.71434 °/min

Orbital period

96.92 mins

BSTAR

0.00034897

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

FLOCK 1C 8, 40040 (Decayed)

FLOCK 1C 9, 40035 (Decayed)

FLOCK 1C 1, 40027 (Decayed)

SL-24 R/B, 40047

FLOCK 1C 6, 40036 (Decayed)

BRITE TORONTO, 40020

UNISAT 6, 40012

FLOCK 1C 11, 40033 (Decayed)

SAUDISAT 4, 40016

DTUSAT 2, 40030

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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.
8 mins	2025-12-09 00:09:50.797Z	10.106° NNE	2025-12-09 00:13:50.797Z	296.201° NW	44.715°	2025-12-09 00:17:50.797Z	196.69° SSW
6 mins	2025-12-09 11:03:50.797Z	151.595° SSE	2025-12-09 11:06:50.797Z	44.203° NE	41.455°	2025-12-09 11:09:50.797Z	356.055° N

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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: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2025-12-08T10:39:47.457Z)

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: 10 hours ago