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 23341.06502749 .00001059 00000-0 22111-3 0 9994
2 00046 66.6888 218.6564 0212128 265.5953 92.0895 14.51168839322867
| Epoch (UTC): | 07 December 2023 01:33:38 |
| Eccentricity: | 0.0212128 |
| inclination: | 66.6888° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 218.6564° |
| argument of perigee: | 265.5953° |
| revolutions per day: | 14.51168839 |
| mean anomaly at epoch: | 92.0895° |
| orbit number at epoch: | 32286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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