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 39444U 13066AE 22182.88615759 .00001009 00000-0 12581-3 0 9994
2 39444 97.6248 156.1387 0056299 347.2471 12.7316 14.83479798463667
| Epoch (UTC): | 01 July 2022 21:16:04 |
| Eccentricity: | 0.0056299 |
| inclination: | 97.6248° |
| perigee height: | 579 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 156.1387° |
| argument of perigee: | 347.2471° |
| revolutions per day: | 14.83479798 |
| mean anomaly at epoch: | 12.7316° |
| orbit number at epoch: | 46366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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