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 23335.13499624 .00003728 00000-0 55859-3 0 9996
2 39161 97.8548 42.5950 0009892 146.3333 213.8507 14.75178884567770
| Epoch (UTC): | 01 December 2023 03:14:23 |
| Eccentricity: | 0.0009892 |
| inclination: | 97.8548° |
| perigee height: | 637 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 42.5950° |
| argument of perigee: | 146.3333° |
| revolutions per day: | 14.75178884 |
| mean anomaly at epoch: | 213.8507° |
| orbit number at epoch: | 56777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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