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 26070U 00006B 22224.71081214 -.00000127 00000-0 -40271-4 0 9997
2 26070 71.0042 320.9915 0016605 359.7969 0.3144 14.15496697163875
| Epoch (UTC): | 12 August 2022 17:03:34 |
| Eccentricity: | 0.0016605 |
| inclination: | 71.0042° |
| perigee height: | 828 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 320.9915° |
| argument of perigee: | 359.7969° |
| revolutions per day: | 14.15496697 |
| mean anomaly at epoch: | 0.3144° |
| orbit number at epoch: | 16387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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