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 40376U 15003A 24282.53253907 .00005426 00000-0 10591-2 0 9996
2 40376 98.1311 287.3326 0001259 93.6567 266.4779 14.63342374517437
| Epoch (UTC): | 08 October 2024 12:46:51 |
| Eccentricity: | 0.0001259 |
| inclination: | 98.1311° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 287.3326° |
| argument of perigee: | 93.6567° |
| revolutions per day: | 14.63342374 |
| mean anomaly at epoch: | 266.4779° |
| orbit number at epoch: | 51743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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