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 22267.09919175 .00000123 00000-0 44473-4 0 9999
2 11 32.8765 183.3351 1467292 250.8518 92.7888 11.86170832715113
| Epoch (UTC): | 24 September 2022 02:22:50 |
| Eccentricity: | 0.1467292 |
| inclination: | 32.8765° |
| perigee height: | 552 km |
| apogee height: | 2935 km |
| right ascension of ascending node: | 183.3351° |
| argument of perigee: | 250.8518° |
| revolutions per day: | 11.86170832 |
| mean anomaly at epoch: | 92.7888° |
| orbit number at epoch: | 71511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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