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 39439U 13066Z 25131.88310521 .00034217 00000-0 12902-2 0 9997
2 39439 97.7425 105.1108 0029903 89.5693 270.8971 15.26557129620536
| Epoch (UTC): | 11 May 2025 21:11:40 |
| Eccentricity: | 0.0029903 |
| inclination: | 97.7425° |
| perigee height: | 465 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 105.1108° |
| argument of perigee: | 89.5693° |
| revolutions per day: | 15.26557129 |
| mean anomaly at epoch: | 270.8971° |
| orbit number at epoch: | 62053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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