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 25397U 98043D 22141.86425692 .00000143 00000-0 82310-4 0 9998
2 25397 98.8160 92.2643 0001593 141.1773 218.9519 14.23752809239648
Epoch (UTC): | 21 May 2022 20:44:31 |
Eccentricity: | 0.0001593 |
inclination: | 98.8160° |
perigee height: | 811 km |
apogee height: | 814 km |
right ascension of ascending node: | 92.2643° |
argument of perigee: | 141.1773° |
revolutions per day: | 14.23752809 |
mean anomaly at epoch: | 218.9519° |
orbit number at epoch: | 23964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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