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 30496U 99025AHJ 24358.08989882 .00011939 00000-0 10892-2 0 9996
2 30496 98.8225 217.2573 0145026 159.5210 201.1900 14.87524686959609
Epoch (UTC): | 23 December 2024 02:09:27 |
Eccentricity: | 0.0145026 |
inclination: | 98.8225° |
perigee height: | 504 km |
apogee height: | 707 km |
right ascension of ascending node: | 217.2573° |
argument of perigee: | 159.5210° |
revolutions per day: | 14.87524686 |
mean anomaly at epoch: | 201.1900° |
orbit number at epoch: | 95960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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