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 25942U 99057C 21113.18606153 .00000096 00000-0 46842-4 0 9993
2 25942 98.7991 95.5248 0099515 14.8290 355.8211 14.36073431127246
Epoch (UTC): | 23 April 2021 04:27:55 |
Eccentricity: | 0.0099515 |
inclination: | 98.7991° |
perigee height: | 700 km |
apogee height: | 842 km |
right ascension of ascending node: | 95.5248° |
argument of perigee: | 14.8290° |
revolutions per day: | 14.36073431 |
mean anomaly at epoch: | 355.8211° |
orbit number at epoch: | 12724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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