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 26100.24032877 +.00000000 +00000-0 -65204-4 0 00002
2 26070 71.0045 31.4941 0014908 139.9911 220.2313 14.15831044 05
| Epoch (UTC): | 10 April 2026 05:46:04 |
| Eccentricity: | 0.0014908 |
| inclination: | 71.0045° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 31.4941° |
| argument of perigee: | 139.9911° |
| revolutions per day: | 14.15831044 |
| mean anomaly at epoch: | 220.2313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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