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 23277.47533080 -.00000007 00000-0 26398-4 0 9999
2 24278 98.5436 241.2029 0350985 133.3402 229.7563 13.53155351339715
| Epoch (UTC): | 04 October 2023 11:24:28 |
| Eccentricity: | 0.0350985 |
| inclination: | 98.5436° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 241.2029° |
| argument of perigee: | 133.3402° |
| revolutions per day: | 13.53155351 |
| mean anomaly at epoch: | 229.7563° |
| orbit number at epoch: | 33971 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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