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 39265U 13055A 25194.20942803 .00027907 -80571-6 42624-3 0 9992
2 39265 80.9416 110.0850 0387603 103.9782 260.4850 14.99186772616414
| Epoch (UTC): | 13 July 2025 05:01:34 |
| Eccentricity: | 0.0387603 |
| inclination: | 80.9416° |
| perigee height: | 300 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 110.0850° |
| argument of perigee: | 103.9782° |
| revolutions per day: | 14.99186772 |
| mean anomaly at epoch: | 260.4850° |
| orbit number at epoch: | 61641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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