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 23336.44293531 .00000100 00000-0 00000-0 0 9996
2 39222 0.0091 340.6753 0000610 278.0224 196.6121 1.00270494 36754
| Epoch (UTC): | 02 December 2023 10:37:49 |
| Eccentricity: | 0.0000610 |
| inclination: | 0.0091° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 340.6753° |
| argument of perigee: | 278.0224° |
| revolutions per day: | 1.00270494 |
| mean anomaly at epoch: | 196.6121° |
| orbit number at epoch: | 3675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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