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 23081.74445468 .00002850 00000-0 44192-3 0 9991
2 39161 97.8806 156.4664 0007991 247.7779 112.2536 14.73897864530444
| Epoch (UTC): | 22 March 2023 17:52:00 |
| Eccentricity: | 0.0007991 |
| inclination: | 97.8806° |
| perigee height: | 643 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 156.4664° |
| argument of perigee: | 247.7779° |
| revolutions per day: | 14.73897864 |
| mean anomaly at epoch: | 112.2536° |
| orbit number at epoch: | 53044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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