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 39161U 13021C 23086.15714812 .00003391 00000-0 52373-3 0 9994
2 39161 97.8741 160.7505 0008907 226.6042 133.4435 14.73933531531098
| Epoch (UTC): | 27 March 2023 03:46:17 |
| Eccentricity: | 0.0008907 |
| inclination: | 97.8741° |
| perigee height: | 642 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 160.7505° |
| argument of perigee: | 226.6042° |
| revolutions per day: | 14.73933531 |
| mean anomaly at epoch: | 133.4435° |
| orbit number at epoch: | 53109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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