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 27845U 03031F 22221.64899472 .00000231 00000-0 12282-3 0 9995
2 27845 98.6724 229.4669 0008433 337.5075 22.5732 14.22573201991322
| Epoch (UTC): | 09 August 2022 15:34:33 |
| Eccentricity: | 0.0008433 |
| inclination: | 98.6724° |
| perigee height: | 810 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 229.4669° |
| argument of perigee: | 337.5075° |
| revolutions per day: | 14.22573201 |
| mean anomaly at epoch: | 22.5732° |
| orbit number at epoch: | 99132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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