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 22305.62875200 0.00000000 00000-0 00000-0 0 09
2 45606 45.0255 154.7090 0000001 75.8305 32.3412 15.98864180 04
| Epoch (UTC): | 01 November 2022 15:05:24 |
| Eccentricity: | 0.0000001 |
| inclination: | 45.0255° |
| perigee height: | 277 km |
| apogee height: | 277 km |
| right ascension of ascending node: | 154.7090° |
| argument of perigee: | 75.8305° |
| revolutions per day: | 15.98864180 |
| mean anomaly at epoch: | 32.3412° |
| 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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