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 13917U 83021B 24284.61876024 .00000231 00000-0 21820-3 0 9991
2 13917 82.9424 61.0035 0027789 333.8857 36.8100 13.77029478 87097
| Epoch (UTC): | 10 October 2024 14:51:00 |
| Eccentricity: | 0.0027789 |
| inclination: | 82.9424° |
| perigee height: | 954 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 61.0035° |
| argument of perigee: | 333.8857° |
| revolutions per day: | 13.77029478 |
| mean anomaly at epoch: | 36.8100° |
| orbit number at epoch: | 8709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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