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 25347.98462113 .00000177 00000-0 81009-4 0 9991
2 39086 98.5503 171.8988 0002893 106.3272 253.8231 14.32757522669084
| Epoch (UTC): | 13 December 2025 23:37:51 |
| Eccentricity: | 0.0002893 |
| inclination: | 98.5503° |
| perigee height: | 780 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 171.8988° |
| argument of perigee: | 106.3272° |
| revolutions per day: | 14.32757522 |
| mean anomaly at epoch: | 253.8231° |
| orbit number at epoch: | 66908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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