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 22180.83240803 .00004473 00000-0 21213-3 0 9995
2 40911 97.4900 184.7340 0011745 319.7694 162.0327 15.19747756374737
Epoch (UTC): | 29 June 2022 19:58:40 |
Eccentricity: | 0.0011745 |
inclination: | 97.4900° |
perigee height: | 498 km |
apogee height: | 514 km |
right ascension of ascending node: | 184.7340° |
argument of perigee: | 319.7694° |
revolutions per day: | 15.19747756 |
mean anomaly at epoch: | 162.0327° |
orbit number at epoch: | 37473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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