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 23270.55348807 .00010160 00000-0 44099-3 0 9997
2 16326 82.5029 108.7172 0007126 285.8386 74.2064 15.22179227 64313
| Epoch (UTC): | 27 September 2023 13:17:01 |
| Eccentricity: | 0.0007126 |
| inclination: | 82.5029° |
| perigee height: | 494 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 108.7172° |
| argument of perigee: | 285.8386° |
| revolutions per day: | 15.22179227 |
| mean anomaly at epoch: | 74.2064° |
| orbit number at epoch: | 6431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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