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 26101.86530294 +.00000000 +00000-0 -98284-4 0 00001
2 26070 71.0046 28.0777 0014837 137.2846 222.9433 14.15830464 01
| Epoch (UTC): | 11 April 2026 20:46:02 |
| Eccentricity: | 0.0014837 |
| inclination: | 71.0046° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 28.0777° |
| argument of perigee: | 137.2846° |
| revolutions per day: | 14.15830464 |
| mean anomaly at epoch: | 222.9433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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