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 40911U 15049N 22142.03752395 .00009880 00000-0 46974-3 0 9997
2 40911 97.4907 146.2355 0015215 88.7210 346.8921 15.19295815368847
Epoch (UTC): | 22 May 2022 00:54:02 |
Eccentricity: | 0.0015215 |
inclination: | 97.4907° |
perigee height: | 497 km |
apogee height: | 518 km |
right ascension of ascending node: | 146.2355° |
argument of perigee: | 88.7210° |
revolutions per day: | 15.19295815 |
mean anomaly at epoch: | 346.8921° |
orbit number at epoch: | 36884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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