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 39086U 13009A 25108.51089352 .00000231 00000-0 10107-3 0 9996
2 39086 98.5543 295.5360 0003152 99.7723 260.3817 14.32684137634795
| Epoch (UTC): | 18 April 2025 12:15:41 |
| Eccentricity: | 0.0003152 |
| inclination: | 98.5543° |
| perigee height: | 780 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 295.5360° |
| argument of perigee: | 99.7723° |
| revolutions per day: | 14.32684137 |
| mean anomaly at epoch: | 260.3817° |
| orbit number at epoch: | 63479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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