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 data is extracted from the following two-line orbital elements,
1 26070U 00006B 25348.87711554 -.00000219 00000-0 -86833-4 0 9997
2 26070 71.0029 276.1634 0018551 305.7047 54.2349 14.15810062336558
| Epoch (UTC): | 14 December 2025 21:03:02 |
| Eccentricity: | 0.0018551 |
| inclination: | 71.0029° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 276.1634° |
| argument of perigee: | 305.7047° |
| revolutions per day: | 14.15810062 |
| mean anomaly at epoch: | 54.2349° |
| orbit number at epoch: | 33655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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