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 17369U 87011A 24337.41107929 .00000169 00000-0 10043-3 0 9992
2 17369 65.0122 21.3962 0020043 257.7979 102.0861 14.31743344 28712
| Epoch (UTC): | 02 December 2024 09:51:57 |
| Eccentricity: | 0.0020043 |
| inclination: | 65.0122° |
| perigee height: | 771 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 21.3962° |
| argument of perigee: | 257.7979° |
| revolutions per day: | 14.31743344 |
| mean anomaly at epoch: | 102.0861° |
| orbit number at epoch: | 2871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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