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 45606U 20029A 22179.88461011 0.00000000 00000-0 00000-0 0 07
2 45606 45.0295 177.4622 0010612 23.0916 336.9080 15.78184295 07
| Epoch (UTC): | 28 June 2022 21:13:50 |
| Eccentricity: | 0.0010612 |
| inclination: | 45.0295° |
| perigee height: | 328 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 177.4622° |
| argument of perigee: | 23.0916° |
| revolutions per day: | 15.78184295 |
| mean anomaly at epoch: | 336.9080° |
| 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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