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 41376U 00055JV 24356.05502477 .00006958 00000-0 28562-2 0 9994
2 41376 98.7446 81.0613 0017516 75.9005 284.4121 14.27266547461845
| Epoch (UTC): | 21 December 2024 01:19:14 |
| Eccentricity: | 0.0017516 |
| inclination: | 98.7446° |
| perigee height: | 788 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 81.0613° |
| argument of perigee: | 75.9005° |
| revolutions per day: | 14.27266547 |
| mean anomaly at epoch: | 284.4121° |
| orbit number at epoch: | 46184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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