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 41786U 16059D 24358.18691975 .00001843 00000-0 31870-3 0 9993
2 41786 98.0646 57.9802 0001921 108.1445 251.9970 14.69544794441272
| Epoch (UTC): | 23 December 2024 04:29:09 |
| Eccentricity: | 0.0001921 |
| inclination: | 98.0646° |
| perigee height: | 661 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 57.9802° |
| argument of perigee: | 108.1445° |
| revolutions per day: | 14.69544794 |
| mean anomaly at epoch: | 251.9970° |
| orbit number at epoch: | 44127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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