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 23340.77156057 .00011910 00000-0 71058-3 0 9999
2 33493 98.2333 7.8719 0014238 180.8306 179.2901 15.11233684809772
| Epoch (UTC): | 06 December 2023 18:31:02 |
| Eccentricity: | 0.0014238 |
| inclination: | 98.2333° |
| perigee height: | 522 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 7.8719° |
| argument of perigee: | 180.8306° |
| revolutions per day: | 15.11233684 |
| mean anomaly at epoch: | 179.2901° |
| orbit number at epoch: | 80977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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