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 14974U 84046B 22146.02925919 .00000053 00000-0 38045-4 0 9991
2 14974 82.9372 240.2589 0044780 354.9051 177.9548 13.76938596910422
Epoch (UTC): | 26 May 2022 00:42:07 |
Eccentricity: | 0.0044780 |
inclination: | 82.9372° |
perigee height: | 942 km |
apogee height: | 1007 km |
right ascension of ascending node: | 240.2589° |
argument of perigee: | 354.9051° |
revolutions per day: | 13.76938596 |
mean anomaly at epoch: | 177.9548° |
orbit number at epoch: | 91042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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