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 40903U 15049E 22179.08452582 .00019165 00000-0 29779-3 0 9999
2 40903 97.1791 237.6340 0011209 85.7252 333.6992 15.53917423380915
Epoch (UTC): | 28 June 2022 02:01:43 |
Eccentricity: | 0.0011209 |
inclination: | 97.1791° |
perigee height: | 398 km |
apogee height: | 413 km |
right ascension of ascending node: | 237.6340° |
argument of perigee: | 85.7252° |
revolutions per day: | 15.53917423 |
mean anomaly at epoch: | 333.6992° |
orbit number at epoch: | 38091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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