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 23339.13244138 .00000238 00000-0 10821-3 0 9993
2 22826 98.8139 24.4539 0007915 275.0559 84.9719 14.30761763575005
| Epoch (UTC): | 05 December 2023 03:10:42 |
| Eccentricity: | 0.0007915 |
| inclination: | 98.8139° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 24.4539° |
| argument of perigee: | 275.0559° |
| revolutions per day: | 14.30761763 |
| mean anomaly at epoch: | 84.9719° |
| orbit number at epoch: | 57500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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