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 25132.39578433 .00000079 00000-0 64295-4 0 9992
2 26070 71.0045 11.3241 0018769 279.1079 80.7920 14.15774621305914
| Epoch (UTC): | 12 May 2025 09:29:55 |
| Eccentricity: | 0.0018769 |
| inclination: | 71.0045° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 11.3241° |
| argument of perigee: | 279.1079° |
| revolutions per day: | 14.15774621 |
| mean anomaly at epoch: | 80.7920° |
| orbit number at epoch: | 30591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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