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 21058.42694276 .00000257 00000-0 25224-4 0 9993
2 22236 82.5068 222.7025 0016401 190.4521 169.6358 14.88015668507197
Epoch (UTC): | 27 February 2021 10:14:47 |
Eccentricity: | 0.0016401 |
inclination: | 82.5068° |
perigee height: | 592 km |
apogee height: | 615 km |
right ascension of ascending node: | 222.7025° |
argument of perigee: | 190.4521° |
revolutions per day: | 14.88015668 |
mean anomaly at epoch: | 169.6358° |
orbit number at epoch: | 50719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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