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 00011U 59001A 24252.71605193 .00001792 00000-0 93939-3 0 9999
2 00011 32.8738 9.0450 1454407 342.0991 13.3126 11.88698645458454
| Epoch (UTC): | 08 September 2024 17:11:06 |
| Eccentricity: | 0.1454407 |
| inclination: | 32.8738° |
| perigee height: | 552 km |
| apogee height: | 2911 km |
| right ascension of ascending node: | 9.0450° |
| argument of perigee: | 342.0991° |
| revolutions per day: | 11.88698645 |
| mean anomaly at epoch: | 13.3126° |
| orbit number at epoch: | 45845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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