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 24277.11872886 .00121605 00000-0 42985-2 0 9991
2 33493 98.1907 334.6310 0010282 229.1062 130.9285 15.28625779855483
| Epoch (UTC): | 03 October 2024 02:50:58 |
| Eccentricity: | 0.0010282 |
| inclination: | 98.1907° |
| perigee height: | 473 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 334.6310° |
| argument of perigee: | 229.1062° |
| revolutions per day: | 15.28625779 |
| mean anomaly at epoch: | 130.9285° |
| orbit number at epoch: | 85548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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