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 30882U 99025AXU 23331.95895633 .00011396 00000-0 15404-2 0 9992
2 30882 98.0456 24.5587 0211888 279.0220 78.7059 14.64800945886577
Epoch (UTC): | 27 November 2023 23:00:53 |
Eccentricity: | 0.0211888 |
inclination: | 98.0456° |
perigee height: | 528 km |
apogee height: | 827 km |
right ascension of ascending node: | 24.5587° |
argument of perigee: | 279.0220° |
revolutions per day: | 14.64800945 |
mean anomaly at epoch: | 78.7059° |
orbit number at epoch: | 88657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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