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 26017.86068994 +.00000000 +00000-0 -96542-4 0 00005
2 26070 71.0001 204.7098 0018891 260.1547 99.7443 14.15812525 08
| Epoch (UTC): | 17 January 2026 20:39:23 |
| Eccentricity: | 0.0018891 |
| inclination: | 71.0001° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 204.7098° |
| argument of perigee: | 260.1547° |
| revolutions per day: | 14.15812525 |
| mean anomaly at epoch: | 99.7443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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