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 16611U 86018A 25196.80728090 .00047422 00000-0 47227-3 0 9999
2 16611 82.4709 324.5386 0003891 88.1231 272.0474 15.65485314157946
| Epoch (UTC): | 15 July 2025 19:22:29 |
| Eccentricity: | 0.0003891 |
| inclination: | 82.4709° |
| perigee height: | 369 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 324.5386° |
| argument of perigee: | 88.1231° |
| revolutions per day: | 15.65485314 |
| mean anomaly at epoch: | 272.0474° |
| orbit number at epoch: | 15794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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