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 25187.92012611 .00042155 00000-0 43290-3 0 9991
2 16611 82.4698 334.0331 0004463 116.6209 243.5508 15.64719022156559
| Epoch (UTC): | 06 July 2025 22:04:58 |
| Eccentricity: | 0.0004463 |
| inclination: | 82.4698° |
| perigee height: | 371 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 334.0331° |
| argument of perigee: | 116.6209° |
| revolutions per day: | 15.64719022 |
| mean anomaly at epoch: | 243.5508° |
| orbit number at epoch: | 15655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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