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 24254.73218973 .00006356 00000-0 12316-2 0 9995
2 00046 66.6901 182.7245 0194470 55.8676 306.0709 14.52510459363318
| Epoch (UTC): | 10 September 2024 17:34:21 |
| Eccentricity: | 0.0194470 |
| inclination: | 66.6901° |
| perigee height: | 579 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 182.7245° |
| argument of perigee: | 55.8676° |
| revolutions per day: | 14.52510459 |
| mean anomaly at epoch: | 306.0709° |
| orbit number at epoch: | 36331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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