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 40910U 15049M 23090.79824083 .00037625 00000-0 11760-2 0 9998
2 40910 97.4689 102.9177 0012287 50.9165 122.0622 15.32990357417014
Epoch (UTC): | 31 March 2023 19:09:28 |
Eccentricity: | 0.0012287 |
inclination: | 97.4689° |
perigee height: | 458 km |
apogee height: | 475 km |
right ascension of ascending node: | 102.9177° |
argument of perigee: | 50.9165° |
revolutions per day: | 15.32990357 |
mean anomaly at epoch: | 122.0622° |
orbit number at epoch: | 41701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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