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 21797U 91081B 22222.10061779 .00000083 00000-0 68111-4 0 9998
2 21797 82.9526 105.9281 0036972 219.4391 298.3815 13.77556395542932
| Epoch (UTC): | 10 August 2022 02:24:53 |
| Eccentricity: | 0.0036972 |
| inclination: | 82.9526° |
| perigee height: | 945 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 105.9281° |
| argument of perigee: | 219.4391° |
| revolutions per day: | 13.77556395 |
| mean anomaly at epoch: | 298.3815° |
| orbit number at epoch: | 54293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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