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 25166.78895673 .00003017 00000-0 30773-3 0 9993
2 39440 97.8500 111.3062 0062523 158.1667 202.2236 14.89969616622362
| Epoch (UTC): | 15 June 2025 18:56:05 |
| Eccentricity: | 0.0062523 |
| inclination: | 97.8500° |
| perigee height: | 554 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 111.3062° |
| argument of perigee: | 158.1667° |
| revolutions per day: | 14.89969616 |
| mean anomaly at epoch: | 202.2236° |
| orbit number at epoch: | 62236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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