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 31114U 07010B 23277.43745795 .00000263 00000-0 14123-3 0 9998
2 31114 98.2966 64.0828 0059435 357.3523 2.7332 14.19628201853809
| Epoch (UTC): | 04 October 2023 10:29:56 |
| Eccentricity: | 0.0059435 |
| inclination: | 98.2966° |
| perigee height: | 784 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 64.0828° |
| argument of perigee: | 357.3523° |
| revolutions per day: | 14.19628201 |
| mean anomaly at epoch: | 2.7332° |
| orbit number at epoch: | 85380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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