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 22178.74979289 .00021419 00000-0 60373-3 0 9996
2 40900 97.3993 196.7831 0006876 240.5941 237.3333 15.36423519376191
Epoch (UTC): | 27 June 2022 17:59:42 |
Eccentricity: | 0.0006876 |
inclination: | 97.3993° |
perigee height: | 452 km |
apogee height: | 461 km |
right ascension of ascending node: | 196.7831° |
argument of perigee: | 240.5941° |
revolutions per day: | 15.36423519 |
mean anomaly at epoch: | 237.3333° |
orbit number at epoch: | 37619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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