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 28645U 05015B 24357.54554278 .00023149 00000-0 16937-2 0 9994
2 28645 0.2353 289.0775 6587519 153.4488 342.5974 3.23254409200099
| Epoch (UTC): | 22 December 2024 13:05:34 |
| Eccentricity: | 0.6587519 |
| inclination: | 0.2353° |
| perigee height: | 215 km |
| apogee height: | 25671 km |
| right ascension of ascending node: | 289.0775° |
| argument of perigee: | 153.4488° |
| revolutions per day: | 3.23254409 |
| mean anomaly at epoch: | 342.5974° |
| orbit number at epoch: | 20009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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