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 23146.95458938 .00004796 00000-0 21859-3 0 9997
2 16326 82.5082 231.6808 0008256 2.5001 357.6273 15.20400519 45810
| Epoch (UTC): | 26 May 2023 22:54:36 |
| Eccentricity: | 0.0008256 |
| inclination: | 82.5082° |
| perigee height: | 499 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 231.6808° |
| argument of perigee: | 2.5001° |
| revolutions per day: | 15.20400519 |
| mean anomaly at epoch: | 357.6273° |
| orbit number at epoch: | 4581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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