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 is defined by the following mean orbital elements,
1 26070U 26017.22482248 +.00000000 +00000-0 -10162-3 0 00000
2 26070 71.0001 206.0468 0018908 261.0187 98.8795 14.15812790 07
| Epoch (UTC): | 17 January 2026 05:23:44 |
| Eccentricity: | 0.0018908 |
| inclination: | 71.0001° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 206.0468° |
| argument of perigee: | 261.0187° |
| revolutions per day: | 14.15812790 |
| mean anomaly at epoch: | 98.8795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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