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 41361U 00055JE 24357.90467439 .00007569 00000-0 38160-2 0 9995
2 41361 98.7668 36.6532 0031468 7.9378 352.2288 14.16307869455764
| Epoch (UTC): | 22 December 2024 21:42:43 |
| Eccentricity: | 0.0031468 |
| inclination: | 98.7668° |
| perigee height: | 815 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 36.6532° |
| argument of perigee: | 7.9378° |
| revolutions per day: | 14.16307869 |
| mean anomaly at epoch: | 352.2288° |
| orbit number at epoch: | 45576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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