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 28096U 03054B 21110.02044050 0.00000000 00000-0 00000-0 0 00
2 28096 63.6755 112.6773 0209577 219.5582 140.4418 13.40867291 01
Epoch (UTC): | 20 April 2021 00:29:26 |
Eccentricity: | 0.0209577 |
inclination: | 63.6755° |
perigee height: | 949 km |
apogee height: | 1263 km |
right ascension of ascending node: | 112.6773° |
argument of perigee: | 219.5582° |
revolutions per day: | 13.40867291 |
mean anomaly at epoch: | 140.4418° |
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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