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 21059.49300569 -.00000003 00000-0 -21496-5 0 9990
2 16986 82.5035 244.7649 0012164 50.3549 309.8750 15.07460767853349
Epoch (UTC): | 28 February 2021 11:49:55 |
Eccentricity: | 0.0012164 |
inclination: | 82.5035° |
perigee height: | 535 km |
apogee height: | 552 km |
right ascension of ascending node: | 244.7649° |
argument of perigee: | 50.3549° |
revolutions per day: | 15.07460767 |
mean anomaly at epoch: | 309.8750° |
orbit number at epoch: | 85334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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