DECAYED

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HODOYOSHI 1, 40299 (Decayed)

Orbit data source: Space-Track

HODOYOSHI 1, 40299 was a payload satellite in LEO that was launched on Thu, 06 Nov 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 embed code

<iframe src="https://www.satcat.com/sats-embedded/40299?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/40299?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40299, 2014-070B

Orbit

Decayed

Last TLE update

2 months ago

Origin

Axelspace (JP)

Manufacturer

AXELSPACE

Mission

Decayed Commercial Imaging

Bus & Motor

HODOYOSHI, Unknown motor

Mass

50 kg wet, 50 kg dry

Launch date (UTC)

2014-11-06 (11 years ago)

Launch vehicle

DNEPR

Launch site

Orenburg, Russia (OREN)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 1.5 m

Radar Cross Section

0.614 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 months ago

0 HODOYOSHI 1
1 40299U 14070B   25071.95296912  .09737855  23840-5  25040-3 0  9994
2 40299  97.0579 141.6986 0009953 253.7226 106.2983 16.45173221577203

Epoch: 2025-03-12T22:52Z

TLE epoch observation values (Epoch: 2025-03-12T22:52:16.531Z)

Latitude

-0.00002°

Longitude

-12.20445°

Altitude

157.176 km

Speed

7.811 km/s

True Right ascension

09h 26m 47s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

155.359 km

Perigee altitude

142.367 km

Semi-major axis

6,527 km

Eccentricity

0.001

Inclination

97.0579°

RAAN

141.6986°

Arg. of periapsis

253.7226°

True anomaly

Unknown

Mean anomaly

106.2983°

Eccentric anomaly

Unknown

Mean motion

4.11598 °/min

Orbital period

87.46 mins

BSTAR

0.0002504

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Other satellites on launch #70 in the year 2014 (2014-11-06 UTC)

ASNARO, 40298

CHUBUSAT 1, 40300 (Decayed)

QSAT-EOS, 40301 (Decayed)

TSUBAME, 40302 (Decayed)

SL-24 R/B, 40303

SL-24 PLAT, 40304 (Decayed)

HODOYOSHI 1 Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out HODOYOSHI 1, 40299 (Decayed) on other resources

View HODOYOSHI 1, 40299 (Decayed) on Celestrak

View HODOYOSHI 1, 40299 (Decayed) on Gunter's Space Page

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