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 23036.94731935 .00000678 00000-0 15680-3 0 9992
2 00046 66.6918 322.1331 0202613 134.0703 227.7290 14.50079235278759
| Epoch (UTC): | 05 February 2023 22:44:08 |
| Eccentricity: | 0.0202613 |
| inclination: | 66.6918° |
| perigee height: | 581 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 322.1331° |
| argument of perigee: | 134.0703° |
| revolutions per day: | 14.50079235 |
| mean anomaly at epoch: | 227.7290° |
| orbit number at epoch: | 27875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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