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 40908U 15049K 22180.84055735 .00002139 00000-0 11510-3 0 9996
2 40908 97.5155 181.2998 0014872 340.4544 139.8484 15.15861760374369
Epoch (UTC): | 29 June 2022 20:10:24 |
Eccentricity: | 0.0014872 |
inclination: | 97.5155° |
perigee height: | 508 km |
apogee height: | 528 km |
right ascension of ascending node: | 181.2998° |
argument of perigee: | 340.4544° |
revolutions per day: | 15.15861760 |
mean anomaly at epoch: | 139.8484° |
orbit number at epoch: | 37436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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