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 28493U 04049B 23083.55068298 .00003433 00000-0 52148-3 0 9998
2 28493 98.1157 189.7326 0005580 114.4068 245.7723 14.74692674981140
Epoch (UTC): | 24 March 2023 13:12:59 |
Eccentricity: | 0.0005580 |
inclination: | 98.1157° |
perigee height: | 642 km |
apogee height: | 650 km |
right ascension of ascending node: | 189.7326° |
argument of perigee: | 114.4068° |
revolutions per day: | 14.74692674 |
mean anomaly at epoch: | 245.7723° |
orbit number at epoch: | 98114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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