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 23344.92452973 .00000603 00000-0 13574-3 0 9992
2 00046 66.6883 208.1958 0212063 262.8087 94.8871 14.51175241323421
| Epoch (UTC): | 10 December 2023 22:11:19 |
| Eccentricity: | 0.0212063 |
| inclination: | 66.6883° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 208.1958° |
| argument of perigee: | 262.8087° |
| revolutions per day: | 14.51175241 |
| mean anomaly at epoch: | 94.8871° |
| orbit number at epoch: | 32342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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