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 21106.24398333 .00000024 00000-0 21337-4 0 9998
2 27386 98.1481 103.4826 0001372 87.2596 341.5607 14.38021001 2135
Epoch (UTC): | 16 April 2021 05:51:20 |
Eccentricity: | 0.0001372 |
inclination: | 98.1481° |
perigee height: | 764 km |
apogee height: | 766 km |
right ascension of ascending node: | 103.4826° |
argument of perigee: | 87.2596° |
revolutions per day: | 14.38021001 |
mean anomaly at epoch: | 341.5607° |
orbit number at epoch: | 213 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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