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 22146.02732429 .00000560 00000-0 27933-3 0 9999
2 11 32.8784 278.2871 1467226 286.7839 57.7212 11.86123380700736
| Epoch (UTC): | 26 May 2022 00:39:20 |
| Eccentricity: | 0.1467226 |
| inclination: | 32.8784° |
| perigee height: | 552 km |
| apogee height: | 2935 km |
| right ascension of ascending node: | 278.2871° |
| argument of perigee: | 286.7839° |
| revolutions per day: | 11.86123380 |
| mean anomaly at epoch: | 57.7212° |
| orbit number at epoch: | 70073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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