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 39446U 13066AG 22182.88225637 .00000844 00000-0 11484-3 0 9995
2 39446 97.6860 146.3219 0069869 43.2890 317.3783 14.79603168462597
| Epoch (UTC): | 01 July 2022 21:10:26 |
| Eccentricity: | 0.0069869 |
| inclination: | 97.6860° |
| perigee height: | 581 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 146.3219° |
| argument of perigee: | 43.2890° |
| revolutions per day: | 14.79603168 |
| mean anomaly at epoch: | 317.3783° |
| orbit number at epoch: | 46259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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