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 39222U 13041A 23081.21556198 .00000073 00000-0 00000+0 0 9997
2 39222 0.0205 146.2306 0000396 130.0806 205.5160 1.00270859 35206
| Epoch (UTC): | 22 March 2023 05:10:24 |
| Eccentricity: | 0.0000396 |
| inclination: | 0.0205° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 146.2306° |
| argument of perigee: | 130.0806° |
| revolutions per day: | 1.00270859 |
| mean anomaly at epoch: | 205.5160° |
| orbit number at epoch: | 3520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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