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 55040U 23001AH 24262.73958923 .00033708 00000-0 10196-2 0 9992
2 55040 97.4187 325.1351 0008530 193.3586 166.7432 15.34096431 95103
| Epoch (UTC): | 18 September 2024 17:45:00 |
| Eccentricity: | 0.0008530 |
| inclination: | 97.4187° |
| perigee height: | 458 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 325.1351° |
| argument of perigee: | 193.3586° |
| revolutions per day: | 15.34096431 |
| mean anomaly at epoch: | 166.7432° |
| orbit number at epoch: | 9510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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