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 43071U 17083B 24357.84299904 .00000137 00000-0 41902-4 0 9991
2 43071 86.3976 187.9494 0002245 72.5141 287.6300 14.34218075366546
| Epoch (UTC): | 22 December 2024 20:13:55 |
| Eccentricity: | 0.0002245 |
| inclination: | 86.3976° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 187.9494° |
| argument of perigee: | 72.5141° |
| revolutions per day: | 14.34218075 |
| mean anomaly at epoch: | 287.6300° |
| orbit number at epoch: | 36654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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