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 23340.11149629 .00000205 00000-0 95860-4 0 9993
2 22826 98.8138 25.4462 0007912 271.8248 88.2028 14.30762254575147
| Epoch (UTC): | 06 December 2023 02:40:33 |
| Eccentricity: | 0.0007912 |
| inclination: | 98.8138° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 25.4462° |
| argument of perigee: | 271.8248° |
| revolutions per day: | 14.30762254 |
| mean anomaly at epoch: | 88.2028° |
| orbit number at epoch: | 57514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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