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 33493U 09002B 23338.12300992 .00012976 00000-0 77517-3 0 9993
2 33493 98.2333 5.0223 0014045 189.2388 170.8584 15.11167149809373
| Epoch (UTC): | 04 December 2023 02:57:08 |
| Eccentricity: | 0.0014045 |
| inclination: | 98.2333° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 5.0223° |
| argument of perigee: | 189.2388° |
| revolutions per day: | 15.11167149 |
| mean anomaly at epoch: | 170.8584° |
| orbit number at epoch: | 80937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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