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 20480U 90013C 22268.43007786 -.00000064 00000-0 -68545-4 0 9996
2 20480 99.0342 65.6950 0539992 347.3970 11.4066 12.83437324528778
| Epoch (UTC): | 25 September 2022 10:19:18 |
| Eccentricity: | 0.0539992 |
| inclination: | 99.0342° |
| perigee height: | 911 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 65.6950° |
| argument of perigee: | 347.3970° |
| revolutions per day: | 12.83437324 |
| mean anomaly at epoch: | 11.4066° |
| orbit number at epoch: | 52877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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