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 04190U 69082BD 22141.33741357 .00010607 00000-0 13487-2 0 9991
2 04190 70.0300 9.1056 0027511 136.3636 223.9697 14.81551658768789
Epoch (UTC): | 21 May 2022 08:05:52 |
Eccentricity: | 0.0027511 |
inclination: | 70.0300° |
perigee height: | 605 km |
apogee height: | 644 km |
right ascension of ascending node: | 9.1056° |
argument of perigee: | 136.3636° |
revolutions per day: | 14.81551658 |
mean anomaly at epoch: | 223.9697° |
orbit number at epoch: | 76878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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