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 23336.39888547 .00015061 00000-0 20267-2 0 9997
2 30882 98.0448 28.9051 0211693 264.9380 92.7631 14.64927654887228
Epoch (UTC): | 02 December 2023 09:34:23 |
Eccentricity: | 0.0211693 |
inclination: | 98.0448° |
perigee height: | 528 km |
apogee height: | 826 km |
right ascension of ascending node: | 28.9051° |
argument of perigee: | 264.9380° |
revolutions per day: | 14.64927654 |
mean anomaly at epoch: | 92.7631° |
orbit number at epoch: | 88722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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