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 22140.49942418 .00000193 00000-0 10862-3 0 9991
2 31114 98.2393 315.5641 0060066 20.6687 339.6900 14.19426496782595
| Epoch (UTC): | 20 May 2022 11:59:10 |
| Eccentricity: | 0.0060066 |
| inclination: | 98.2393° |
| perigee height: | 784 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 315.5641° |
| argument of perigee: | 20.6687° |
| revolutions per day: | 14.19426496 |
| mean anomaly at epoch: | 339.6900° |
| orbit number at epoch: | 78259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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