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 22826U 93061D 24340.12666650 .00000450 00000-0 18803-3 0 9996
2 22826 98.7608 34.3704 0007886 285.3651 74.6660 14.31073501627346
| Epoch (UTC): | 05 December 2024 03:02:23 |
| Eccentricity: | 0.0007886 |
| inclination: | 98.7608° |
| perigee height: | 782 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 34.3704° |
| argument of perigee: | 285.3651° |
| revolutions per day: | 14.31073501 |
| mean anomaly at epoch: | 74.6660° |
| orbit number at epoch: | 62734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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