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 40900U 15049B 22178.87275910 .00021388 00000-0 60277-3 0 9998
2 40900 97.3993 196.9067 0006953 238.6420 198.9902 15.36428751376210
Epoch (UTC): | 27 June 2022 20:56:46 |
Eccentricity: | 0.0006953 |
inclination: | 97.3993° |
perigee height: | 452 km |
apogee height: | 461 km |
right ascension of ascending node: | 196.9067° |
argument of perigee: | 238.6420° |
revolutions per day: | 15.36428751 |
mean anomaly at epoch: | 198.9902° |
orbit number at epoch: | 37621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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