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 23333.83159144 .00006189 00000-0 72912-3 0 9999
2 39446 97.7577 283.5660 0064035 155.3898 205.0395 14.83652802539568
| Epoch (UTC): | 29 November 2023 19:57:29 |
| Eccentricity: | 0.0064035 |
| inclination: | 97.7577° |
| perigee height: | 573 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 283.5660° |
| argument of perigee: | 155.3898° |
| revolutions per day: | 14.83652802 |
| mean anomaly at epoch: | 205.0395° |
| orbit number at epoch: | 53956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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