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 35483U 97051QD 22222.76986569 .00007812 00000-0 16497-2 0 9998
2 35483 86.4299 237.5037 0036866 157.9893 202.2910 14.58835878696498
Epoch (UTC): | 10 August 2022 18:28:36 |
Eccentricity: | 0.0036866 |
inclination: | 86.4299° |
perigee height: | 671 km |
apogee height: | 723 km |
right ascension of ascending node: | 237.5037° |
argument of perigee: | 157.9893° |
revolutions per day: | 14.58835878 |
mean anomaly at epoch: | 202.2910° |
orbit number at epoch: | 69649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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