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 22138.75373581 .00003423 00000-0 20714-3 0 9993
2 28647 56.9973 270.3491 0118997 330.1065 29.3212 15.07567498165493
| Epoch (UTC): | 18 May 2022 18:05:22 |
| Eccentricity: | 0.0118997 |
| inclination: | 56.9973° |
| perigee height: | 461 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 270.3491° |
| argument of perigee: | 330.1065° |
| revolutions per day: | 15.07567498 |
| mean anomaly at epoch: | 29.3212° |
| orbit number at epoch: | 16549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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