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 21063.74122831 .00000185 00000-0 10229-4 0 9997
2 16986 82.5031 240.6248 0012135 36.6716 323.5340 15.07461989853981
Epoch (UTC): | 04 March 2021 17:47:22 |
Eccentricity: | 0.0012135 |
inclination: | 82.5031° |
perigee height: | 535 km |
apogee height: | 552 km |
right ascension of ascending node: | 240.6248° |
argument of perigee: | 36.6716° |
revolutions per day: | 15.07461989 |
mean anomaly at epoch: | 323.5340° |
orbit number at epoch: | 85398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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