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 24278.32242480 .00024664 00000-0 93009-3 0 9993
2 28647 57.0053 294.9053 0097620 114.2978 246.8300 15.22600889297111
| Epoch (UTC): | 04 October 2024 07:44:17 |
| Eccentricity: | 0.0097620 |
| inclination: | 57.0053° |
| perigee height: | 431 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 294.9053° |
| argument of perigee: | 114.2978° |
| revolutions per day: | 15.22600889 |
| mean anomaly at epoch: | 246.8300° |
| orbit number at epoch: | 29711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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