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 25198.40521202 .00052226 00000-0 51673-3 0 9991
2 16611 82.4704 322.8307 0003742 82.0364 278.1320 15.65638506158479
| Epoch (UTC): | 17 July 2025 09:43:30 |
| Eccentricity: | 0.0003742 |
| inclination: | 82.4704° |
| perigee height: | 369 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 322.8307° |
| argument of perigee: | 82.0364° |
| revolutions per day: | 15.65638506 |
| mean anomaly at epoch: | 278.1320° |
| orbit number at epoch: | 15847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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