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 22175.90064508 .00000002 00000-0 40614-4 0 9998
2 24278 98.5153 198.5664 0349215 263.9751 92.1497 13.53116381276618
| Epoch (UTC): | 24 June 2022 21:36:55 |
| Eccentricity: | 0.0349215 |
| inclination: | 98.5153° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 198.5664° |
| argument of perigee: | 263.9751° |
| revolutions per day: | 13.53116381 |
| mean anomaly at epoch: | 92.1497° |
| orbit number at epoch: | 27661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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