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 23087.17545161 .00003607 00000-0 55666-3 0 9994
2 39161 97.8778 161.7424 0008728 223.6976 136.3616 14.73940012531245
| Epoch (UTC): | 28 March 2023 04:12:39 |
| Eccentricity: | 0.0008728 |
| inclination: | 97.8778° |
| perigee height: | 642 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 161.7424° |
| argument of perigee: | 223.6976° |
| revolutions per day: | 14.73940012 |
| mean anomaly at epoch: | 136.3616° |
| orbit number at epoch: | 53124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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