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 42849U 17042AA 23083.80871513 .00006540 00000-0 60728-3 0 9991
2 42849 97.3944 291.3958 0008815 126.8580 233.3451 14.94678251310163
Epoch (UTC): | 24 March 2023 19:24:32 |
Eccentricity: | 0.0008815 |
inclination: | 97.3944° |
perigee height: | 577 km |
apogee height: | 589 km |
right ascension of ascending node: | 291.3958° |
argument of perigee: | 126.8580° |
revolutions per day: | 14.94678251 |
mean anomaly at epoch: | 233.3451° |
orbit number at epoch: | 31016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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