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 31254U 99025BML 23330.66945970 .00003057 00000-0 10009-2 0 9994
2 31254 98.5639 20.2472 0159659 259.2986 232.2448 14.32206575868068
| Epoch (UTC): | 26 November 2023 16:04:01 |
| Eccentricity: | 0.0159659 |
| inclination: | 98.5639° |
| perigee height: | 670 km |
| apogee height: | 899 km |
| right ascension of ascending node: | 20.2472° |
| argument of perigee: | 259.2986° |
| revolutions per day: | 14.32206575 |
| mean anomaly at epoch: | 232.2448° |
| orbit number at epoch: | 86806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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