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 16625U 86014F 21057.90400800 .00001214 00000-0 11989-3 0 9994
2 16625 63.2974 247.7938 0929337 80.1917 290.2647 13.47291813 79726
Epoch (UTC): | 26 February 2021 21:41:46 |
Eccentricity: | 0.0929337 |
inclination: | 63.2974° |
perigee height: | 389 km |
apogee height: | 1775 km |
right ascension of ascending node: | 247.7938° |
argument of perigee: | 80.1917° |
revolutions per day: | 13.47291813 |
mean anomaly at epoch: | 290.2647° |
orbit number at epoch: | 7972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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