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 25194.39905677 .00026708 00000-0 90447-3 0 9991
2 39439 97.7442 170.1191 0022947 223.2070 136.7370 15.30305397630083
| Epoch (UTC): | 13 July 2025 09:34:38 |
| Eccentricity: | 0.0022947 |
| inclination: | 97.7442° |
| perigee height: | 459 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 170.1191° |
| argument of perigee: | 223.2070° |
| revolutions per day: | 15.30305397 |
| mean anomaly at epoch: | 136.7370° |
| orbit number at epoch: | 63008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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