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 42257U 95015FX 24357.38228788 .00208424 00000-0 13204-1 0 9998
2 42257 98.7349 148.5692 0008878 118.4029 241.8091 15.07877596481411
Epoch (UTC): | 22 December 2024 09:10:29 |
Eccentricity: | 0.0008878 |
inclination: | 98.7349° |
perigee height: | 536 km |
apogee height: | 549 km |
right ascension of ascending node: | 148.5692° |
argument of perigee: | 118.4029° |
revolutions per day: | 15.07877596 |
mean anomaly at epoch: | 241.8091° |
orbit number at epoch: | 48141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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