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 25119.10239043 .00008344 00000-0 84930-3 0 9992
2 39440 97.8473 63.9665 0061330 318.3401 41.3153 14.89585780616463
| Epoch (UTC): | 29 April 2025 02:27:26 |
| Eccentricity: | 0.0061330 |
| inclination: | 97.8473° |
| perigee height: | 556 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 63.9665° |
| argument of perigee: | 318.3401° |
| revolutions per day: | 14.89585780 |
| mean anomaly at epoch: | 41.3153° |
| orbit number at epoch: | 61646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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