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 16986U 86074A 21055.77580921 .00000128 00000-0 64524-5 0 9994
2 16986 82.5041 248.3874 0012091 61.7978 298.4470 15.07460701852784
Epoch (UTC): | 24 February 2021 18:37:09 |
Eccentricity: | 0.0012091 |
inclination: | 82.5041° |
perigee height: | 535 km |
apogee height: | 552 km |
right ascension of ascending node: | 248.3874° |
argument of perigee: | 61.7978° |
revolutions per day: | 15.07460701 |
mean anomaly at epoch: | 298.4470° |
orbit number at epoch: | 85278 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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