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 23344.61177757 .00007627 00000-0 45601-3 0 9991
2 33493 98.2330 12.0043 0014556 167.0700 193.0904 15.11304423810347
| Epoch (UTC): | 10 December 2023 14:40:57 |
| Eccentricity: | 0.0014556 |
| inclination: | 98.2330° |
| perigee height: | 522 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 12.0043° |
| argument of perigee: | 167.0700° |
| revolutions per day: | 15.11304423 |
| mean anomaly at epoch: | 193.0904° |
| orbit number at epoch: | 81034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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