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 22144.72886865 .00000143 00000-0 85082-4 0 9996
2 31114 98.2396 319.4997 0059833 8.3441 351.8717 14.19427679783199
| Epoch (UTC): | 24 May 2022 17:29:34 |
| Eccentricity: | 0.0059833 |
| inclination: | 98.2396° |
| perigee height: | 784 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 319.4997° |
| argument of perigee: | 8.3441° |
| revolutions per day: | 14.19427679 |
| mean anomaly at epoch: | 351.8717° |
| orbit number at epoch: | 78319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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