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 06139U 70025MV 23027.12554869 .00001834 00000-0 13550-2 0 9999
2 06139 99.0009 274.0753 0072145 149.6812 210.8553 13.95369797656062
| Epoch (UTC): | 27 January 2023 03:00:47 |
| Eccentricity: | 0.0072145 |
| inclination: | 99.0009° |
| perigee height: | 857 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 274.0753° |
| argument of perigee: | 149.6812° |
| revolutions per day: | 13.95369797 |
| mean anomaly at epoch: | 210.8553° |
| orbit number at epoch: | 65606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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