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 39446U 13066AG 23341.38499843 .00002222 00000-0 26543-3 0 9994
2 39446 97.7580 290.9065 0064584 131.0233 229.6590 14.83722667540092
| Epoch (UTC): | 07 December 2023 09:14:23 |
| Eccentricity: | 0.0064584 |
| inclination: | 97.7580° |
| perigee height: | 572 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 290.9065° |
| argument of perigee: | 131.0233° |
| revolutions per day: | 14.83722667 |
| mean anomaly at epoch: | 229.6590° |
| orbit number at epoch: | 54009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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