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 23151.37712798 .00005003 00000-0 26972-3 0 9992
2 28647 56.9936 167.0188 0107704 294.4887 64.4952 15.11644999222509
| Epoch (UTC): | 31 May 2023 09:03:03 |
| Eccentricity: | 0.0107704 |
| inclination: | 56.9936° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 167.0188° |
| argument of perigee: | 294.4887° |
| revolutions per day: | 15.11644999 |
| mean anomaly at epoch: | 64.4952° |
| orbit number at epoch: | 22250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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