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 28706U 90017C 22181.21289560 .00000526 00000-0 45277-3 0 9998
2 28706 83.0885 93.5561 0081017 193.1129 166.7928 13.83345839857577
Epoch (UTC): | 30 June 2022 05:06:34 |
Eccentricity: | 0.0081017 |
inclination: | 83.0885° |
perigee height: | 892 km |
apogee height: | 1011 km |
right ascension of ascending node: | 93.5561° |
argument of perigee: | 193.1129° |
revolutions per day: | 13.83345839 |
mean anomaly at epoch: | 166.7928° |
orbit number at epoch: | 85757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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