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 25189.55470213 .00000177 00000-0 11443-3 0 9994
2 26070 71.0017 251.1462 0017195 200.4556 159.5880 14.15780613314009
| Epoch (UTC): | 08 July 2025 13:18:46 |
| Eccentricity: | 0.0017195 |
| inclination: | 71.0017° |
| perigee height: | 827 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 251.1462° |
| argument of perigee: | 200.4556° |
| revolutions per day: | 14.15780613 |
| mean anomaly at epoch: | 159.5880° |
| orbit number at epoch: | 31400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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