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 22176.08236840 .00005861 00000-0 27713-3 0 9996
2 40911 97.4902 180.0201 0012237 337.8291 93.0052 15.19708424374013
Epoch (UTC): | 25 June 2022 01:58:36 |
Eccentricity: | 0.0012237 |
inclination: | 97.4902° |
perigee height: | 498 km |
apogee height: | 515 km |
right ascension of ascending node: | 180.0201° |
argument of perigee: | 337.8291° |
revolutions per day: | 15.19708424 |
mean anomaly at epoch: | 93.0052° |
orbit number at epoch: | 37401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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