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 24280.82660840 .00004685 00000-0 90640-3 0 9998
2 00046 66.6891 111.8472 0195718 35.7999 325.6046 14.52724343367103
| Epoch (UTC): | 06 October 2024 19:50:18 |
| Eccentricity: | 0.0195718 |
| inclination: | 66.6891° |
| perigee height: | 578 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 111.8472° |
| argument of perigee: | 35.7999° |
| revolutions per day: | 14.52724343 |
| mean anomaly at epoch: | 325.6046° |
| orbit number at epoch: | 36710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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