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 22279.44211287 .00001132 00000-0 24048-3 0 9992
2 00046 66.6890 293.4917 0214524 225.4888 132.8518 14.49829410260993
| Epoch (UTC): | 06 October 2022 10:36:38 |
| Eccentricity: | 0.0214524 |
| inclination: | 66.6890° |
| perigee height: | 574 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 293.4917° |
| argument of perigee: | 225.4888° |
| revolutions per day: | 14.49829410 |
| mean anomaly at epoch: | 132.8518° |
| orbit number at epoch: | 26099 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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