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 21056.08380337 0.00000000 00000-0 00000-0 0 07
2 26906 63.4559 111.5662 0470584 339.5030 20.4970 13.44074974 05
Epoch (UTC): | 25 February 2021 02:00:40 |
Eccentricity: | 0.0470584 |
inclination: | 63.4559° |
perigee height: | 742 km |
apogee height: | 1446 km |
right ascension of ascending node: | 111.5662° |
argument of perigee: | 339.5030° |
revolutions per day: | 13.44074974 |
mean anomaly at epoch: | 20.4970° |
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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