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 24338.12333840 .00074297 00000-0 19263-2 0 9999
2 33493 98.1783 42.1582 0007826 21.1046 339.0518 15.38710374864836
| Epoch (UTC): | 03 December 2024 02:57:36 |
| Eccentricity: | 0.0007826 |
| inclination: | 98.1783° |
| perigee height: | 444 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 42.1582° |
| argument of perigee: | 21.1046° |
| revolutions per day: | 15.38710374 |
| mean anomaly at epoch: | 339.0518° |
| orbit number at epoch: | 86483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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