DECAYED
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ONGLAISAT, 62299 (Decayed)

Orbit data source: Space-Track

ONGLAISAT, 62299 was a Japanese payload satellite 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
62299, 1998-067XF
Orbit
Decayed
Last TLE update
2 months ago
Origin
Manufacturer
TASA/TOK
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
1998-11-20 (26 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, 0.3 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 months ago
0 ONGLAISAT
1 62299U 98067XF  25059.17504503  .06741359  11906-4  34511-2 0  9996
2 62299  51.6164 116.6321 0004997 356.7632   3.3353 16.19717774 12655
Epoch: 2025-02-28T04:12Z
Definitive object data (Epoch: 2025-02-28T04:12:03.89Z)
Latitude
-0.00002°
Longitude
-104.62377°
Altitude
217.787 km
Speed
7.779 km/s
True Right ascension
07h 46m 31s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
224.143 km
Perigee altitude
217.548 km
Semi-major axis
6,598.982 km
Eccentricity
0.0004997
Inclination
51.6164°
RAAN
116.6321°
Arg. of periapsis
356.7632°
True anomaly
3.33863°
Mean anomaly
3.3353°
Eccentric anomaly
3.33697°
Mean motion
4.04881 °/min
BSTAR
0.0034511
Orbital period
88.91 mins
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ONGLAISAT Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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