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 25138.89593222 -.00000209 00000-0 -82050-4 0 9992
2 26070 71.0036 357.6582 0018886 270.3893 89.5066 14.15774194306830
| Epoch (UTC): | 18 May 2025 21:30:08 |
| Eccentricity: | 0.0018886 |
| inclination: | 71.0036° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 357.6582° |
| argument of perigee: | 270.3893° |
| revolutions per day: | 14.15774194 |
| mean anomaly at epoch: | 89.5066° |
| orbit number at epoch: | 30683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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