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 42759U 17034B 25175.53629021 .00044364 00000-0 43395-3 0 9998
2 42759 43.0054 232.6126 0019962 30.8957 329.3079 15.65145011444943
| Epoch (UTC): | 24 June 2025 12:52:15 |
| Eccentricity: | 0.0019962 |
| inclination: | 43.0054° |
| perigee height: | 359 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 232.6126° |
| argument of perigee: | 30.8957° |
| revolutions per day: | 15.65145011 |
| mean anomaly at epoch: | 329.3079° |
| orbit number at epoch: | 44494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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