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 16262U 85108A 25191.54837294 .00008003 00000-0 20356-3 0 9999
2 16262 82.4619 212.6609 0008404 142.2766 217.9070 15.39388527164658
| Epoch (UTC): | 10 July 2025 13:09:39 |
| Eccentricity: | 0.0008404 |
| inclination: | 82.4619° |
| perigee height: | 442 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 212.6609° |
| argument of perigee: | 142.2766° |
| revolutions per day: | 15.39388527 |
| mean anomaly at epoch: | 217.9070° |
| orbit number at epoch: | 16465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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