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 25187.87023761 .00006122 00000-0 22635-3 0 9994
2 16986 82.5289 125.7179 0006957 19.5300 340.6204 15.27488439 93713
| Epoch (UTC): | 06 July 2025 20:53:08 |
| Eccentricity: | 0.0006957 |
| inclination: | 82.5289° |
| perigee height: | 478 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 125.7179° |
| argument of perigee: | 19.5300° |
| revolutions per day: | 15.27488439 |
| mean anomaly at epoch: | 340.6204° |
| orbit number at epoch: | 9371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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