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 39444U 13066AE 23277.45997913 .00009016 00000-0 96769-3 0 9994
2 39444 97.6851 238.0809 0049787 272.4109 87.1408 14.87905037531889
| Epoch (UTC): | 04 October 2023 11:02:22 |
| Eccentricity: | 0.0049787 |
| inclination: | 97.6851° |
| perigee height: | 570 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 238.0809° |
| argument of perigee: | 272.4109° |
| revolutions per day: | 14.87905037 |
| mean anomaly at epoch: | 87.1408° |
| orbit number at epoch: | 53188 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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