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 16591U 86014A 23258.78839643 0.00015700 00000-0 83753-3 0 04
2 16591 63.2840 227.0653 0868359 93.2879 266.7120 13.71411460 01
| Epoch (UTC): | 15 September 2023 18:55:17 |
| Eccentricity: | 0.0868359 |
| inclination: | 63.2840° |
| perigee height: | 354 km |
| apogee height: | 1635 km |
| right ascension of ascending node: | 227.0653° |
| argument of perigee: | 93.2879° |
| revolutions per day: | 13.71411460 |
| mean anomaly at epoch: | 266.7120° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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