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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 (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: 2 days ago

TLE from 2 days ago

0 HODOYOSHI 3
1 40015U 14033F   26171.41846669  .00000763  00000-0  93914-4 0  9998
2 40015  97.6421 334.3289 0032388 346.5693  13.4657 14.85393755648108

Epoch: 2026-06-20T10:02Z

TLE epoch observation values (Epoch: 2026-06-20T10:02:35.522Z)

Latitude

-0.00001°

Longitude

-84.95248°

Altitude

593.368 km

Speed

7.575 km/s

True Right ascension

22h 17m 18s

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

21:42:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

632.004 km

Perigee altitude

586.741 km

Semi-major axis

6,987.509 km

Eccentricity

0.00324

Inclination

97.6421°

RAAN

334.3289°

Arg. of periapsis

346.5693°

True anomaly

13.55247°

Mean anomaly

13.4657°

Eccentric anomaly

13.50905°

Mean motion

3.71586 °/min

Orbital period

96.88 mins

BSTAR

0.000093914

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

DUCHIFAT 1, 40021

POLYITAN 1, 40042

FLOCK 1C 7, 40026 (Decayed)

POPSAT HIP 1, 40028

BUGSAT 1, 40014

TABLETSAT AURORA, 40017

AEROCUBE 6A, 40045

FLOCK 1C 5, 40038 (Decayed)

FLOCK 1C 11, 40033 (Decayed)

KAZEOSAT 2, 40010

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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.
7 mins	2026-06-22 10:40:47.139Z	151.252° SSE	2026-06-22 10:43:47.139Z	63.456° ENE	41.365°	2026-06-22 10:47:47.139Z	354.857° N
6 mins	2026-06-23 00:03:47.139Z	354.654° N	2026-06-23 00:05:47.139Z	305.104° NW	39.55°	2026-06-23 00:09:47.139Z	209.305° SW

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T10:02:35.522Z)

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: 2 days ago