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 16326U 85113A 25191.44363200 .00011693 00000-0 22713-3 0 9994
2 16326 82.4943 168.1220 0007752 112.7166 247.4904 15.47441732164161
| Epoch (UTC): | 10 July 2025 10:38:49 |
| Eccentricity: | 0.0007752 |
| inclination: | 82.4943° |
| perigee height: | 419 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 168.1220° |
| argument of perigee: | 112.7166° |
| revolutions per day: | 15.47441732 |
| mean anomaly at epoch: | 247.4904° |
| orbit number at epoch: | 16416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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