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 11327U 79030B 22148.81033163 .00000051 00000-0 36275-4 0 9998
2 11327 82.9525 34.4847 0028105 159.5432 244.7594 13.76969960167546
| Epoch (UTC): | 28 May 2022 19:26:52 |
| Eccentricity: | 0.0028105 |
| inclination: | 82.9525° |
| perigee height: | 954 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 34.4847° |
| argument of perigee: | 159.5432° |
| revolutions per day: | 13.76969960 |
| mean anomaly at epoch: | 244.7594° |
| orbit number at epoch: | 16754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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