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 39430U 13066Q 25163.55400508 .00001526 00000-0 24311-3 0 9997
2 39430 97.6832 22.0366 0132304 182.2901 177.7716 14.67645978615848
| Epoch (UTC): | 12 June 2025 13:17:46 |
| Eccentricity: | 0.0132304 |
| inclination: | 97.6832° |
| perigee height: | 575 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 22.0366° |
| argument of perigee: | 182.2901° |
| revolutions per day: | 14.67645978 |
| mean anomaly at epoch: | 177.7716° |
| orbit number at epoch: | 61584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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