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 42661U 75052MW 24355.69069505 .00001936 00000-0 60748-3 0 9994
2 42661 98.7878 345.8915 0005048 106.8588 253.3154 14.41733532581578
| Epoch (UTC): | 20 December 2024 16:34:36 |
| Eccentricity: | 0.0005048 |
| inclination: | 98.7878° |
| perigee height: | 749 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 345.8915° |
| argument of perigee: | 106.8588° |
| revolutions per day: | 14.41733532 |
| mean anomaly at epoch: | 253.3154° |
| orbit number at epoch: | 58157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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