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 27386U 02009A 21105.25869836 .00000024 00000-0 21278-4 0 9993
2 27386 98.1480 102.5478 0001379 87.6999 283.3925 14.38020889 1997
Epoch (UTC): | 15 April 2021 06:12:31 |
Eccentricity: | 0.0001379 |
inclination: | 98.1480° |
perigee height: | 764 km |
apogee height: | 766 km |
right ascension of ascending node: | 102.5478° |
argument of perigee: | 87.6999° |
revolutions per day: | 14.38020889 |
mean anomaly at epoch: | 283.3925° |
orbit number at epoch: | 199 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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