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 11086U 78100C 22138.47250830 .00000043 00000-0 44485-3 0 9992
2 11086 82.5481 167.5852 0013416 70.7008 57.2703 11.96735066902589
| Epoch (UTC): | 18 May 2022 11:20:24 |
| Eccentricity: | 0.0013416 |
| inclination: | 82.5481° |
| perigee height: | 1684 km |
| apogee height: | 1706 km |
| right ascension of ascending node: | 167.5852° |
| argument of perigee: | 70.7008° |
| revolutions per day: | 11.96735066 |
| mean anomaly at epoch: | 57.2703° |
| orbit number at epoch: | 90258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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