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.
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62295 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast 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 12140Epoch: 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
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
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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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.YODAKA 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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