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 42299U 95015HR 24357.05924033 .00032125 00000-0 77600-2 0 9998
2 42299 98.7105 34.1079 0018603 172.6791 187.4679 14.52896802481395
Epoch (UTC): | 22 December 2024 01:25:18 |
Eccentricity: | 0.0018603 |
inclination: | 98.7105° |
perigee height: | 703 km |
apogee height: | 729 km |
right ascension of ascending node: | 34.1079° |
argument of perigee: | 172.6791° |
revolutions per day: | 14.52896802 |
mean anomaly at epoch: | 187.4679° |
orbit number at epoch: | 48139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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