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 16864U 86052B 22227.40529879 .00000096 00000-0 38105-4 0 9991
2 16864 74.0279 205.6302 0033491 202.5929 157.3754 14.40747292894130
Epoch (UTC): | 15 August 2022 09:43:37 |
Eccentricity: | 0.0033491 |
inclination: | 74.0279° |
perigee height: | 732 km |
apogee height: | 780 km |
right ascension of ascending node: | 205.6302° |
argument of perigee: | 202.5929° |
revolutions per day: | 14.40747292 |
mean anomaly at epoch: | 157.3754° |
orbit number at epoch: | 89413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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