View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 107U 61013A 23334.76922332 .00004974 00000-0 63124-3 0 9991
2 107 28.7856 243.3620 0527610 140.1568 223.8982 14.13725801143983
Epoch (UTC): | 30 November 2023 18:27:40 |
Eccentricity: | 0.0527610 |
inclination: | 28.7856° |
perigee height: | 465 km |
apogee height: | 1228 km |
right ascension of ascending node: | 243.3620° |
argument of perigee: | 140.1568° |
revolutions per day: | 14.13725801 |
mean anomaly at epoch: | 223.8982° |
orbit number at epoch: | 14398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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