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 23331.80828222 .00005419 00000-0 63985-3 0 9999
2 39446 97.7570 281.6002 0063809 161.9566 198.3934 14.83626710538676
| Epoch (UTC): | 27 November 2023 19:23:55 |
| Eccentricity: | 0.0063809 |
| inclination: | 97.7570° |
| perigee height: | 573 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 281.6002° |
| argument of perigee: | 161.9566° |
| revolutions per day: | 14.83626710 |
| mean anomaly at epoch: | 198.3934° |
| orbit number at epoch: | 53867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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