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 41051U 00055J 24356.49278947 .00007335 00000-0 29613-2 0 9992
2 41051 98.7808 89.3357 0014798 66.1172 294.1558 14.28123549469338
| Epoch (UTC): | 21 December 2024 11:49:37 |
| Eccentricity: | 0.0014798 |
| inclination: | 98.7808° |
| perigee height: | 787 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 89.3357° |
| argument of perigee: | 66.1172° |
| revolutions per day: | 14.28123549 |
| mean anomaly at epoch: | 294.1558° |
| orbit number at epoch: | 46933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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