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 41378U 00055JX 24357.50920729 .00005400 00000-0 27687-2 0 9999
2 41378 98.6603 16.0491 0043293 256.4602 103.1746 14.15314864459595
| Epoch (UTC): | 22 December 2024 12:13:15 |
| Eccentricity: | 0.0043293 |
| inclination: | 98.6603° |
| perigee height: | 810 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 16.0491° |
| argument of perigee: | 256.4602° |
| revolutions per day: | 14.15314864 |
| mean anomaly at epoch: | 103.1746° |
| orbit number at epoch: | 45959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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