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 26906U 01040B 21090.82888783 0.00000000 00000-0 00000-0 0 05
2 26906 63.4493 22.2693 0471166 339.4249 20.5751 13.44077320 08
Epoch (UTC): | 31 March 2021 19:53:35 |
Eccentricity: | 0.0471166 |
inclination: | 63.4493° |
perigee height: | 742 km |
apogee height: | 1446 km |
right ascension of ascending node: | 22.2693° |
argument of perigee: | 339.4249° |
revolutions per day: | 13.44077320 |
mean anomaly at epoch: | 20.5751° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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