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 25198.89771531 .00007453 00000-0 16919-3 0 9994
2 39452 87.3423 179.4500 0003205 92.0542 268.1082 15.42845391654576
| Epoch (UTC): | 17 July 2025 21:32:42 |
| Eccentricity: | 0.0003205 |
| inclination: | 87.3423° |
| perigee height: | 435 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 179.4500° |
| argument of perigee: | 92.0542° |
| revolutions per day: | 15.42845391 |
| mean anomaly at epoch: | 268.1082° |
| orbit number at epoch: | 65457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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