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.
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62299 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
TASA/TOK
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 1 year ago
TLE from 1 year 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 12655Epoch: 2025-02-28T04:12Z
TLE epoch observation values (Epoch: 2025-02-28T04:12:03.890Z)
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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
224.143 km
Perigee altitude
217.548 km
Semi-major axis
6,598.982 km
Eccentricity
0.0005
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
Orbital period
88.91 mins
BSTAR
0.0034511
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Other satellites on launch #67 in the year 1998 (1998-11-20 UTC)
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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.ONGLAISAT Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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