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 22143.66064457 .00003196 00000-0 19402-3 0 9997
2 28647 56.9969 250.3461 0119762 339.1790 20.4391 15.07608394166232
| Epoch (UTC): | 23 May 2022 15:51:19 |
| Eccentricity: | 0.0119762 |
| inclination: | 56.9969° |
| perigee height: | 460 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 250.3461° |
| argument of perigee: | 339.1790° |
| revolutions per day: | 15.07608394 |
| mean anomaly at epoch: | 20.4391° |
| orbit number at epoch: | 16623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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