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 22147.81403590 .00000313 00000-0 83462-4 0 9993
2 00046 66.6901 289.4423 0214186 320.6892 37.8829 14.49688567241916
| Epoch (UTC): | 27 May 2022 19:32:12 |
| Eccentricity: | 0.0214186 |
| inclination: | 66.6901° |
| perigee height: | 574 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 289.4423° |
| argument of perigee: | 320.6892° |
| revolutions per day: | 14.49688567 |
| mean anomaly at epoch: | 37.8829° |
| orbit number at epoch: | 24191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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