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 16986U 86074A 25193.70039753 .00005970 00000-0 22028-3 0 9997
2 16986 82.5298 119.8794 0006230 359.8701 0.2535 15.27557651 94607
| Epoch (UTC): | 12 July 2025 16:48:34 |
| Eccentricity: | 0.0006230 |
| inclination: | 82.5298° |
| perigee height: | 479 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 119.8794° |
| argument of perigee: | 359.8701° |
| revolutions per day: | 15.27557651 |
| mean anomaly at epoch: | 0.2535° |
| orbit number at epoch: | 9460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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