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 14506U 83113A 22224.78811340 .00000116 00000-0 63010-4 0 9998
2 14506 98.2880 49.7049 0012329 63.5966 307.2723 14.28280674 14919
| Epoch (UTC): | 12 August 2022 18:54:52 |
| Eccentricity: | 0.0012329 |
| inclination: | 98.2880° |
| perigee height: | 788 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 49.7049° |
| argument of perigee: | 63.5966° |
| revolutions per day: | 14.28280674 |
| mean anomaly at epoch: | 307.2723° |
| orbit number at epoch: | 1491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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