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 00046U 60007B 22148.50393434 .00000296 00000-0 80182-4 0 9991
2 00046 66.6901 287.5769 0214235 320.1850 38.3702 14.49689224242011
| Epoch (UTC): | 28 May 2022 12:05:39 |
| Eccentricity: | 0.0214235 |
| inclination: | 66.6901° |
| perigee height: | 574 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 287.5769° |
| argument of perigee: | 320.1850° |
| revolutions per day: | 14.49689224 |
| mean anomaly at epoch: | 38.3702° |
| orbit number at epoch: | 24201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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