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 23266.58940420 .00011235 00000-0 55120-3 0 9998
2 28647 56.9952 53.8430 0112125 141.0909 219.8270 15.13235034239936
| Epoch (UTC): | 23 September 2023 14:08:44 |
| Eccentricity: | 0.0112125 |
| inclination: | 56.9952° |
| perigee height: | 449 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 53.8430° |
| argument of perigee: | 141.0909° |
| revolutions per day: | 15.13235034 |
| mean anomaly at epoch: | 219.8270° |
| orbit number at epoch: | 23993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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