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 26622U 00075D 24357.59846432 -.00000426 00000-0 -36668-3 0 9998
2 26622 95.4081 195.7281 0715418 201.7551 224.6884 13.04869609146637
| Epoch (UTC): | 22 December 2024 14:21:47 |
| Eccentricity: | 0.0715418 |
| inclination: | 95.4081° |
| perigee height: | 698 km |
| apogee height: | 1788 km |
| right ascension of ascending node: | 195.7281° |
| argument of perigee: | 201.7551° |
| revolutions per day: | 13.04869609 |
| mean anomaly at epoch: | 224.6884° |
| orbit number at epoch: | 14663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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