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 28647U 05016B 22230.57599966 .00001779 00000-0 11330-3 0 9999
2 28647 56.9945 255.8506 0123826 132.5788 228.5779 15.08121191179347
| Epoch (UTC): | 18 August 2022 13:49:26 |
| Eccentricity: | 0.0123826 |
| inclination: | 56.9945° |
| perigee height: | 456 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 255.8506° |
| argument of perigee: | 132.5788° |
| revolutions per day: | 15.08121191 |
| mean anomaly at epoch: | 228.5779° |
| orbit number at epoch: | 17934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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