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 11U 59001A 24281.19938572 .00002070 00000-0 10866-2 0 9990
2 11 32.8656 261.5413 1453922 143.7621 227.0850 11.88787301803588
| Epoch (UTC): | 07 October 2024 04:47:06 |
| Eccentricity: | 0.1453922 |
| inclination: | 32.8656° |
| perigee height: | 552 km |
| apogee height: | 2910 km |
| right ascension of ascending node: | 261.5413° |
| argument of perigee: | 143.7621° |
| revolutions per day: | 11.88787301 |
| mean anomaly at epoch: | 227.0850° |
| orbit number at epoch: | 80358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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