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 33683U 99025DFU 22331.52844918 .00004390 00000-0 11840-2 0 9992
2 33683 98.2490 179.6306 0070988 330.3982 29.3201 14.46900052769087
| Epoch (UTC): | 27 November 2022 12:40:58 |
| Eccentricity: | 0.0070988 |
| inclination: | 98.2490° |
| perigee height: | 685 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 179.6306° |
| argument of perigee: | 330.3982° |
| revolutions per day: | 14.46900052 |
| mean anomaly at epoch: | 29.3201° |
| orbit number at epoch: | 76908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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