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 23152.36909283 .00005968 00000-0 31831-3 0 9999
2 28647 56.9936 162.9496 0107750 296.3972 62.6040 15.11658098222651
| Epoch (UTC): | 01 June 2023 08:51:29 |
| Eccentricity: | 0.0107750 |
| inclination: | 56.9936° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 162.9496° |
| argument of perigee: | 296.3972° |
| revolutions per day: | 15.11658098 |
| mean anomaly at epoch: | 62.6040° |
| orbit number at epoch: | 22265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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