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 41925U 17003J 24357.86937389 .00000620 00000-0 21417-3 0 9992
2 41925 86.3961 314.5084 0002466 81.3522 278.7953 14.34214359415681
| Epoch (UTC): | 22 December 2024 20:51:53 |
| Eccentricity: | 0.0002466 |
| inclination: | 86.3961° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 314.5084° |
| argument of perigee: | 81.3522° |
| revolutions per day: | 14.34214359 |
| mean anomaly at epoch: | 278.7953° |
| orbit number at epoch: | 41568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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