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 35233U 99025DQR 23033.16136458 .00002716 00000-0 11717-2 0 9991
2 35233 98.8071 108.0299 0054285 91.2772 299.0174 14.24538013762235
| Epoch (UTC): | 02 February 2023 03:52:21 |
| Eccentricity: | 0.0054285 |
| inclination: | 98.8071° |
| perigee height: | 771 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 108.0299° |
| argument of perigee: | 91.2772° |
| revolutions per day: | 14.24538013 |
| mean anomaly at epoch: | 299.0174° |
| orbit number at epoch: | 76223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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