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 22139.99947351 .00000332 00000-0 12302-3 0 9990
2 27386 98.1820 122.4439 0001324 86.7328 340.2342 14.38121234 59444
Epoch (UTC): | 19 May 2022 23:59:14 |
Eccentricity: | 0.0001324 |
inclination: | 98.1820° |
perigee height: | 764 km |
apogee height: | 765 km |
right ascension of ascending node: | 122.4439° |
argument of perigee: | 86.7328° |
revolutions per day: | 14.38121234 |
mean anomaly at epoch: | 340.2342° |
orbit number at epoch: | 5944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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