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 40910U 15049M 22178.79298332 .00007619 00000-0 32473-3 0 9991
2 40910 97.4721 185.7960 0011166 304.6759 230.1977 15.23181887374750
Epoch (UTC): | 27 June 2022 19:01:53 |
Eccentricity: | 0.0011166 |
inclination: | 97.4721° |
perigee height: | 488 km |
apogee height: | 504 km |
right ascension of ascending node: | 185.7960° |
argument of perigee: | 304.6759° |
revolutions per day: | 15.23181887 |
mean anomaly at epoch: | 230.1977° |
orbit number at epoch: | 37475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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