DECAYED

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TSUBAME, 40302 (Decayed)

Orbit data source: Space-Track

TSUBAME, 40302 was a Japanese 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/40302?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/40302?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40302, 2014-070E

Orbit

Decayed

Last TLE update

6 months ago

Origin

Institute of Science Tokyo (JP / JPN)

Manufacturer

TITech

Mission

Decayed Amateur Astronomy

Bus & Motor

TSUBAME, Unknown motor

Mass

43 kg wet, 43 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, 1.2 m

Radar Cross Section

0.370 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 6 months ago

0 TSUBAME
1 40302U 14070E   24304.92016278  .14555910  24222-5  75248-3 0  9995
2 40302  97.0699 313.9580 0008498 243.4054 116.6377 16.42023614554487

Epoch: 2024-10-30T22:05Z

Definitive object data (Epoch: 2024-10-30T22:05:02.064Z)

Latitude

-0.00002°

Longitude

-57.01134°

Altitude

166.184 km

Speed

7.805 km/s

True Right ascension

20h 55m 49s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

162.769 km

Perigee altitude

151.662 km

Semi-major axis

6,535.352 km

Eccentricity

0.0008498

Inclination

97.0699°

RAAN

313.958°

Arg. of periapsis

243.4054°

True anomaly

116.7247°

Mean anomaly

116.6377°

Eccentric anomaly

116.68121°

Mean motion

4.10809 °/min

BSTAR

0.00075248

Orbital period

87.63 mins

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

ASNARO, 40298

HODOYOSHI 1, 40299 (Decayed)

CHUBUSAT 1, 40300 (Decayed)

QSAT-EOS, 40301 (Decayed)

SL-24 R/B, 40303

SL-24 PLAT, 40304 (Decayed)

TSUBAME Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out TSUBAME, 40302 (Decayed) on other resources

View TSUBAME, 40302 (Decayed) on Celestrak

View TSUBAME, 40302 (Decayed) on Gunter's Space Page

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