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 35933U 09051C 22267.57081272 .00000528 00000-0 12834-3 0 9995
2 35933 98.5494 127.7845 0006756 110.5068 249.6855 14.56972004690601
| Epoch (UTC): | 24 September 2022 13:41:58 |
| Eccentricity: | 0.0006756 |
| inclination: | 98.5494° |
| perigee height: | 698 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 127.7845° |
| argument of perigee: | 110.5068° |
| revolutions per day: | 14.56972004 |
| mean anomaly at epoch: | 249.6855° |
| orbit number at epoch: | 69060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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