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 22178.56260169 -.00000009 00000-0 29676-4 0 9997
2 24278 98.5152 200.8625 0349225 257.0466 99.1465 13.53116583276974
| Epoch (UTC): | 27 June 2022 13:30:08 |
| Eccentricity: | 0.0349225 |
| inclination: | 98.5152° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 200.8625° |
| argument of perigee: | 257.0466° |
| revolutions per day: | 13.53116583 |
| mean anomaly at epoch: | 99.1465° |
| orbit number at epoch: | 27697 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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