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 24357.85228168 .00003040 00000-0 57984-3 0 9997
2 00046 66.6897 262.4991 0201864 337.8797 21.3690 14.53238239378292
| Epoch (UTC): | 22 December 2024 20:27:17 |
| Eccentricity: | 0.0201864 |
| inclination: | 66.6897° |
| perigee height: | 572 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 262.4991° |
| argument of perigee: | 337.8797° |
| revolutions per day: | 14.53238239 |
| mean anomaly at epoch: | 21.3690° |
| orbit number at epoch: | 37829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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