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 20670U 90057A 24358.10372593 .00000086 00000-0 62617-4 0 9998
2 20670 82.5459 349.1819 0016493 158.0910 202.0959 13.84836600743013
Epoch (UTC): | 23 December 2024 02:29:21 |
Eccentricity: | 0.0016493 |
inclination: | 82.5459° |
perigee height: | 935 km |
apogee height: | 959 km |
right ascension of ascending node: | 349.1819° |
argument of perigee: | 158.0910° |
revolutions per day: | 13.84836600 |
mean anomaly at epoch: | 202.0959° |
orbit number at epoch: | 74301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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