DECAYED
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YODAKA, 62295 (Decayed)

Orbit data source: Space-Track

YODAKA, 62295 was a payload satellite owned by ArkEdge (JP) in LEO that was delivered to the ISS. 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
Identifier
62295, 1998-067XB
Orbit
Decayed
Country
Flag of JPJP / JPN
Related business
Manufacturer
ArkEdge
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
1998-11-20 (27 years ago)
Launch vehicle
FALCON 9
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 YODAKA
1 62295U 98067XB  25055.56990578  .07916730  12268-4  15183-2 0  9996
2 62295  51.6144 133.7689 0008198 359.2402   0.8607 16.30980865 12140
Epoch: 2025-02-24T13:40Z
TLE epoch observation values (Epoch: 2025-02-24T13:40:39.859Z)
Latitude
-0°
Longitude
133.91657°
Altitude
185.285 km
Speed
7.8 km/s
True Right ascension
08h 55m 04s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
00:11:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
195.82 km
Perigee altitude
185.05 km
Semi-major axis
6,568.572 km
Eccentricity
0.00082
Inclination
51.6144°
RAAN
133.7689°
Arg. of periapsis
359.2402°
True anomaly
0.86211°
Mean anomaly
0.8607°
Eccentric anomaly
0.86141°
Mean motion
4.07696 °/min
Orbital period
88.3 mins
BSTAR
0.0015183
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