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 16182U 85097B 25199.48348940 .00000150 00000-0 99068-4 0 9995
2 16182 71.0025 273.6058 0009635 257.1406 190.4673 14.16554941 54069
| Epoch (UTC): | 18 July 2025 11:36:13 |
| Eccentricity: | 0.0009635 |
| inclination: | 71.0025° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 273.6058° |
| argument of perigee: | 257.1406° |
| revolutions per day: | 14.16554941 |
| mean anomaly at epoch: | 190.4673° |
| orbit number at epoch: | 5406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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