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 22147.47800388 .00000146 00000-0 86685-4 0 9990
2 31114 98.2396 322.0580 0059644 0.3863 359.7351 14.19429012783584
| Epoch (UTC): | 27 May 2022 11:28:19 |
| Eccentricity: | 0.0059644 |
| inclination: | 98.2396° |
| perigee height: | 784 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 322.0580° |
| argument of perigee: | 0.3863° |
| revolutions per day: | 14.19429012 |
| mean anomaly at epoch: | 359.7351° |
| orbit number at epoch: | 78358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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