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 30873U 99025AXK 24279.82189432 .00002319 00000-0 10754-2 0 9991
2 30873 98.6099 286.4976 0111086 97.3155 264.0662 14.18435088910539
Epoch (UTC): | 05 October 2024 19:43:31 |
Eccentricity: | 0.0111086 |
inclination: | 98.6099° |
perigee height: | 750 km |
apogee height: | 911 km |
right ascension of ascending node: | 286.4976° |
argument of perigee: | 97.3155° |
revolutions per day: | 14.18435088 |
mean anomaly at epoch: | 264.0662° |
orbit number at epoch: | 91053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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