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 22136.59351327 .00000068 00000-0 49588-4 0 9991
2 25397 98.8158 86.9811 0001286 149.3761 210.7492 14.23750843238890
Epoch (UTC): | 16 May 2022 14:14:39 |
Eccentricity: | 0.0001286 |
inclination: | 98.8158° |
perigee height: | 812 km |
apogee height: | 813 km |
right ascension of ascending node: | 86.9811° |
argument of perigee: | 149.3761° |
revolutions per day: | 14.23750843 |
mean anomaly at epoch: | 210.7492° |
orbit number at epoch: | 23889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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