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 23332.03071318 .00019342 00000-0 11606-2 0 9994
2 33493 98.2336 358.4694 0013640 211.3889 148.6526 15.10909988808457
| Epoch (UTC): | 28 November 2023 00:44:13 |
| Eccentricity: | 0.0013640 |
| inclination: | 98.2336° |
| perigee height: | 524 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 358.4694° |
| argument of perigee: | 211.3889° |
| revolutions per day: | 15.10909988 |
| mean anomaly at epoch: | 148.6526° |
| orbit number at epoch: | 80845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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