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 23335.89601805 .00002561 00000-0 50268-3 0 9994
2 00046 66.6904 232.6655 0212194 269.3014 88.3779 14.51153630322116
| Epoch (UTC): | 01 December 2023 21:30:15 |
| Eccentricity: | 0.0212194 |
| inclination: | 66.6904° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 232.6655° |
| argument of perigee: | 269.3014° |
| revolutions per day: | 14.51153630 |
| mean anomaly at epoch: | 88.3779° |
| orbit number at epoch: | 32211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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