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 16728U 86037B 22222.46172847 .00000131 00000-0 11711-3 0 9996
2 16728 82.9554 23.1298 0030438 345.3247 41.3592 13.76777158819037
Epoch (UTC): | 10 August 2022 11:04:53 |
Eccentricity: | 0.0030438 |
inclination: | 82.9554° |
perigee height: | 953 km |
apogee height: | 998 km |
right ascension of ascending node: | 23.1298° |
argument of perigee: | 345.3247° |
revolutions per day: | 13.76777158 |
mean anomaly at epoch: | 41.3592° |
orbit number at epoch: | 81903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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