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 23081.56384122 .00007892 00000-0 38497-3 0 9995
2 40908 97.5262 84.9338 0015971 126.8686 350.6371 15.18465835414649
Epoch (UTC): | 22 March 2023 13:31:55 |
Eccentricity: | 0.0015971 |
inclination: | 97.5262° |
perigee height: | 499 km |
apogee height: | 521 km |
right ascension of ascending node: | 84.9338° |
argument of perigee: | 126.8686° |
revolutions per day: | 15.18465835 |
mean anomaly at epoch: | 350.6371° |
orbit number at epoch: | 41464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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