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 24277.21694520 .00000908 00000-0 43894-3 0 9997
2 31114 98.3489 47.0684 0059495 15.0832 345.2103 14.19907774905576
| Epoch (UTC): | 03 October 2024 05:12:24 |
| Eccentricity: | 0.0059495 |
| inclination: | 98.3489° |
| perigee height: | 783 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 47.0684° |
| argument of perigee: | 15.0832° |
| revolutions per day: | 14.19907774 |
| mean anomaly at epoch: | 345.2103° |
| orbit number at epoch: | 90557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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