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 26021.53459177 +.00000000 +00000-0 +30956-4 0 00007
2 26070 71.0002 196.9847 0018764 255.0942 104.8103 14.15812620 01
| Epoch (UTC): | 21 January 2026 12:49:48 |
| Eccentricity: | 0.0018764 |
| inclination: | 71.0002° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 196.9847° |
| argument of perigee: | 255.0942° |
| revolutions per day: | 14.15812620 |
| mean anomaly at epoch: | 104.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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