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 35684U 09041D 23333.57482965 .00001869 00000-0 24531-3 0 9992
2 35684 98.2661 9.5833 0047115 89.2681 271.3929 14.80794297773483
| Epoch (UTC): | 29 November 2023 13:47:45 |
| Eccentricity: | 0.0047115 |
| inclination: | 98.2661° |
| perigee height: | 594 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 9.5833° |
| argument of perigee: | 89.2681° |
| revolutions per day: | 14.80794297 |
| mean anomaly at epoch: | 271.3929° |
| orbit number at epoch: | 77348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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