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 28188U 04008B 24357.83759638 .00009212 00000-0 12009-2 0 9997
2 28188 49.4835 200.5637 4978450 150.1854 251.1556 5.67448443403665
| Epoch (UTC): | 22 December 2024 20:06:08 |
| Eccentricity: | 0.4978450 |
| inclination: | 49.4835° |
| perigee height: | 289 km |
| apogee height: | 13509 km |
| right ascension of ascending node: | 200.5637° |
| argument of perigee: | 150.1854° |
| revolutions per day: | 5.67448443 |
| mean anomaly at epoch: | 251.1556° |
| orbit number at epoch: | 40366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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