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 23032.43459569 .00000081 00000-0 56510-4 0 9993
2 31114 98.2580 194.9706 0059397 351.3134 8.7010 14.19493439819048
| Epoch (UTC): | 01 February 2023 10:25:49 |
| Eccentricity: | 0.0059397 |
| inclination: | 98.2580° |
| perigee height: | 784 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 194.9706° |
| argument of perigee: | 351.3134° |
| revolutions per day: | 14.19493439 |
| mean anomaly at epoch: | 8.7010° |
| orbit number at epoch: | 81904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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