YOTSUBA-KULOVER, 65941 (Decayed)
Orbit data source: Space-Track
YOTSUBA-KULOVER, 65941 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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65941 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 YOTSUBA-KULOVER
1 65941U 98067XN 26106.72901255 .06739310 12393-4 74116-3 0 9994
2 65941 51.6034 215.6287 0009820 317.4833 42.5431 16.36262631 29573Epoch: 2026-04-16T17:29Z
TLE epoch observation values (Epoch: 2026-04-16T17:29:46.684Z)
Latitude
0.00003°
Longitude
108.31183°
Altitude
171.789 km
Speed
7.807 km/s
True Right ascension
14h 22m 30s
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
16:50:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
182.732 km
Perigee altitude
169.859 km
Semi-major axis
6,554.433 km
Eccentricity
0.00098
Inclination
51.6034°
RAAN
215.6287°
Arg. of periapsis
317.4833°
True anomaly
42.61925°
Mean anomaly
42.5431°
Eccentric anomaly
42.58117°
Mean motion
4.09016 °/min
Orbital period
88.02 mins
BSTAR
0.00074116
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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.YOTSUBA-KULOVER 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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