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 54349U 22151CU 24276.95904710 .00004685 00000-0 18181-2 0 9996
2 54349 98.7032 287.5044 0111938 117.7309 243.5278 14.26978627 97916
| Epoch (UTC): | 02 October 2024 23:01:01 |
| Eccentricity: | 0.0111938 |
| inclination: | 98.7032° |
| perigee height: | 721 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 287.5044° |
| argument of perigee: | 117.7309° |
| revolutions per day: | 14.26978627 |
| mean anomaly at epoch: | 243.5278° |
| orbit number at epoch: | 9791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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