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 20303U 89085B 22142.74767922 .00020513 00000-0 53181-3 0 9995
2 20303 35.6378 251.3239 0080786 340.3973 19.3659 15.34800072776503
| Epoch (UTC): | 22 May 2022 17:56:39 |
| Eccentricity: | 0.0080786 |
| inclination: | 35.6378° |
| perigee height: | 406 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 251.3239° |
| argument of perigee: | 340.3973° |
| revolutions per day: | 15.34800072 |
| mean anomaly at epoch: | 19.3659° |
| orbit number at epoch: | 77650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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