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 22825U 93061C 22270.09742677 .00000059 00000-0 40678-4 0 9996
2 22825 98.8797 303.2482 0009458 113.2188 246.9991 14.30193419512688
| Epoch (UTC): | 27 September 2022 02:20:17 |
| Eccentricity: | 0.0009458 |
| inclination: | 98.8797° |
| perigee height: | 784 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 303.2482° |
| argument of perigee: | 113.2188° |
| revolutions per day: | 14.30193419 |
| mean anomaly at epoch: | 246.9991° |
| orbit number at epoch: | 51268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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