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 24284.36203400 .00028114 00000-0 10496-2 0 9995
2 28647 57.0071 269.7111 0096831 124.7365 236.2846 15.22920232298032
| Epoch (UTC): | 10 October 2024 08:41:19 |
| Eccentricity: | 0.0096831 |
| inclination: | 57.0071° |
| perigee height: | 430 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 269.7111° |
| argument of perigee: | 124.7365° |
| revolutions per day: | 15.22920232 |
| mean anomaly at epoch: | 236.2846° |
| orbit number at epoch: | 29803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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