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 26694U 01005A 22263.95464111 0.00000000 00000-0 00000-0 0 02
2 26694 10.0760 39.4064 0008623 97.5255 262.5846 0.98738430 06
| Epoch (UTC): | 20 September 2022 22:54:40 |
| Eccentricity: | 0.0008623 |
| inclination: | 10.0760° |
| perigee height: | 36185 km |
| apogee height: | 36258 km |
| right ascension of ascending node: | 39.4064° |
| argument of perigee: | 97.5255° |
| revolutions per day: | 0.98738430 |
| mean anomaly at epoch: | 262.5846° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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