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 24278U 96046B 22179.52386667 -.00000015 00000-0 23744-4 0 9993
2 24278 98.5151 201.6916 0349236 254.5439 101.6881 13.53116619277106
| Epoch (UTC): | 28 June 2022 12:34:22 |
| Eccentricity: | 0.0349236 |
| inclination: | 98.5151° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 201.6916° |
| argument of perigee: | 254.5439° |
| revolutions per day: | 13.53116619 |
| mean anomaly at epoch: | 101.6881° |
| orbit number at epoch: | 27710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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