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 40025U 14033R 22136.56895049 .00003811 00000-0 39728-3 0 9997
2 40025 97.9597 73.7271 0012752 154.9707 205.2131 14.90331891429015
Epoch (UTC): | 16 May 2022 13:39:17 |
Eccentricity: | 0.0012752 |
inclination: | 97.9597° |
perigee height: | 588 km |
apogee height: | 606 km |
right ascension of ascending node: | 73.7271° |
argument of perigee: | 154.9707° |
revolutions per day: | 14.90331891 |
mean anomaly at epoch: | 205.2131° |
orbit number at epoch: | 42901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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