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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 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: 23 hours ago

TLE from 23 hours ago

0 HODOYOSHI 3
1 40015U 14033F   26078.18043826  .00001157  00000-0  14007-3 0  9995
2 40015  97.6317 244.8998 0031643 291.8873  67.8978 14.85165022634264

Epoch: 2026-03-19T04:19Z

TLE epoch observation values (Epoch: 2026-03-19T04:19:49.865Z)

Latitude

-0.00012°

Longitude

3.20849°

Altitude

607.839 km

Speed

7.56 km/s

True Right ascension

16h 19m 35s

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

07:56:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

632.203 km

Perigee altitude

587.977 km

Semi-major axis

6,988.227 km

Eccentricity

0.00316

Inclination

97.6317°

RAAN

244.8998°

Arg. of periapsis

291.8873°

True anomaly

68.23425°

Mean anomaly

67.8978°

Eccentric anomaly

68.06598°

Mean motion

3.71529 °/min

Orbital period

96.9 mins

BSTAR

0.00014007

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

TABLETSAT AURORA, 40017

FLOCK 1C 11, 40033 (Decayed)

SL-24 DEB, 40048 (Decayed)

FLOCK 1C 3, 40041 (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.
7 mins	2026-03-20 11:10:35.757Z	173.334° S	2026-03-20 11:13:35.757Z	211.566° SW	43.244°	2026-03-20 11:17:35.757Z	343.643° N
5 mins	2026-03-20 22:58:35.757Z	60.733° ENE	2026-03-20 23:00:35.757Z	95.577° ESE	19.169°	2026-03-20 23:03:35.757Z	140.681° SSE
5 mins	2026-03-21 00:34:35.757Z	334.683° NNW	2026-03-21 00:36:35.757Z	287.313° WNW	29.077°	2026-03-21 00:39:35.757Z	230.8° WSW

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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: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-03-19T04:19:49.865Z)

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: 23 hours ago