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 22236U 92080A 21055.19916215 .00000290 00000-0 28878-4 0 9999
2 22236 82.5065 225.7530 0016111 201.3698 158.6849 14.88014020506714
Epoch (UTC): | 24 February 2021 04:46:47 |
Eccentricity: | 0.0016111 |
inclination: | 82.5065° |
perigee height: | 593 km |
apogee height: | 615 km |
right ascension of ascending node: | 225.7530° |
argument of perigee: | 201.3698° |
revolutions per day: | 14.88014020 |
mean anomaly at epoch: | 158.6849° |
orbit number at epoch: | 50671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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