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 35111U 99025DKP 24356.10374241 .00001145 00000-0 67280-3 0 9995
2 35111 99.5024 49.3877 0022855 132.4131 227.8976 14.10202674591167
| Epoch (UTC): | 21 December 2024 02:29:23 |
| Eccentricity: | 0.0022855 |
| inclination: | 99.5024° |
| perigee height: | 842 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 49.3877° |
| argument of perigee: | 132.4131° |
| revolutions per day: | 14.10202674 |
| mean anomaly at epoch: | 227.8976° |
| orbit number at epoch: | 59116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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