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 41265U 00055FR 24355.97484794 .00007684 00000-0 36749-2 0 9995
2 41265 98.6366 0.2570 0032199 312.5298 47.3160 14.19078555462756
| Epoch (UTC): | 20 December 2024 23:23:46 |
| Eccentricity: | 0.0032199 |
| inclination: | 98.6366° |
| perigee height: | 805 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 0.2570° |
| argument of perigee: | 312.5298° |
| revolutions per day: | 14.19078555 |
| mean anomaly at epoch: | 47.3160° |
| orbit number at epoch: | 46275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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