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 26018.92046922 +.00000000 +00000-0 -76430-4 0 00004
2 26070 71.0001 202.4814 0018869 258.7190 101.1812 14.15812250 04
| Epoch (UTC): | 18 January 2026 22:05:28 |
| Eccentricity: | 0.0018869 |
| inclination: | 71.0001° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 202.4814° |
| argument of perigee: | 258.7190° |
| revolutions per day: | 14.15812250 |
| mean anomaly at epoch: | 101.1812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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