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 30745U 99025ATF 24357.81768787 .00059883 00000-0 87394-2 0 9993
2 30745 99.2371 116.5848 0014460 182.3019 329.6643 14.75393049929440
Epoch (UTC): | 22 December 2024 19:37:28 |
Eccentricity: | 0.0014460 |
inclination: | 99.2371° |
perigee height: | 634 km |
apogee height: | 654 km |
right ascension of ascending node: | 116.5848° |
argument of perigee: | 182.3019° |
revolutions per day: | 14.75393049 |
mean anomaly at epoch: | 329.6643° |
orbit number at epoch: | 92944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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