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 39440U 13066AA 25138.84992636 .00004515 00000-0 46072-3 0 9999
2 39440 97.8484 83.5646 0060491 251.4211 108.0430 14.89792963619404
| Epoch (UTC): | 18 May 2025 20:23:53 |
| Eccentricity: | 0.0060491 |
| inclination: | 97.8484° |
| perigee height: | 556 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 83.5646° |
| argument of perigee: | 251.4211° |
| revolutions per day: | 14.89792963 |
| mean anomaly at epoch: | 108.0430° |
| orbit number at epoch: | 61940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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