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 24280.81074495 .00000845 00000-0 40998-3 0 9992
2 31114 98.3494 50.4597 0059299 4.6186 355.5526 14.19912981906076
| Epoch (UTC): | 06 October 2024 19:27:28 |
| Eccentricity: | 0.0059299 |
| inclination: | 98.3494° |
| perigee height: | 783 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 50.4597° |
| argument of perigee: | 4.6186° |
| revolutions per day: | 14.19912981 |
| mean anomaly at epoch: | 355.5526° |
| orbit number at epoch: | 90607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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