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 45875U 20046C 22224.89893406 0.00010191 00000-0 69260-3 0 01
2 45875 53.9798 229.7632 0004052 132.1929 227.8070 15.05890636 00
| Epoch (UTC): | 12 August 2022 21:34:27 |
| Eccentricity: | 0.0004052 |
| inclination: | 53.9798° |
| perigee height: | 546 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 229.7632° |
| argument of perigee: | 132.1929° |
| revolutions per day: | 15.05890636 |
| mean anomaly at epoch: | 227.8070° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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