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 22011.45804818 0.00000000 00000-0 00000-0 0 01
2 45606 45.0410 88.9419 0002086 288.0397 71.9598 15.78192697 03
| Epoch (UTC): | 11 January 2022 10:59:35 |
| Eccentricity: | 0.0002086 |
| inclination: | 45.0410° |
| perigee height: | 334 km |
| apogee height: | 337 km |
| right ascension of ascending node: | 88.9419° |
| argument of perigee: | 288.0397° |
| revolutions per day: | 15.78192697 |
| mean anomaly at epoch: | 71.9598° |
| 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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