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 23340.40725610 .00000856 00000-0 43546-3 0 9998
2 11 32.8753 334.3962 1460263 210.2293 140.5541 11.87423321767207
| Epoch (UTC): | 06 December 2023 09:46:26 |
| Eccentricity: | 0.1460263 |
| inclination: | 32.8753° |
| perigee height: | 552 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 334.3962° |
| argument of perigee: | 210.2293° |
| revolutions per day: | 11.87423321 |
| mean anomaly at epoch: | 140.5541° |
| orbit number at epoch: | 76720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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