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 22825U 93061C 24349.42633941 .00000273 00000-0 12160-3 0 9997
2 22825 98.7650 43.8724 0007339 271.9733 88.0608 14.30680392628651
Epoch (UTC): | 14 December 2024 10:13:55 |
Eccentricity: | 0.0007339 |
inclination: | 98.7650° |
perigee height: | 784 km |
apogee height: | 795 km |
right ascension of ascending node: | 43.8724° |
argument of perigee: | 271.9733° |
revolutions per day: | 14.30680392 |
mean anomaly at epoch: | 88.0608° |
orbit number at epoch: | 62865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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