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 39452U 13067B 25196.95187001 .00006393 00000-0 14512-3 0 9991
2 39452 87.3422 180.1611 0003194 91.4553 268.7069 15.42817286654279
| Epoch (UTC): | 15 July 2025 22:50:41 |
| Eccentricity: | 0.0003194 |
| inclination: | 87.3422° |
| perigee height: | 435 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 180.1611° |
| argument of perigee: | 91.4553° |
| revolutions per day: | 15.42817286 |
| mean anomaly at epoch: | 268.7069° |
| orbit number at epoch: | 65427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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