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 26065.40925463 +.00000000 +00000-0 +63491-4 0 00007
2 26070 71.0012 104.7358 0017008 194.8070 165.2557 14.15825561 00
| Epoch (UTC): | 06 March 2026 09:49:19 |
| Eccentricity: | 0.0017008 |
| inclination: | 71.0012° |
| perigee height: | 827 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 104.7358° |
| argument of perigee: | 194.8070° |
| revolutions per day: | 14.15825561 |
| mean anomaly at epoch: | 165.2557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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