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 39026U 12072A 22147.55166294 .00014692 00000-0 41350-3 0 9994
2 39026 97.2667 138.5226 0029078 231.0972 128.7679 15.36138687525770
| Epoch (UTC): | 27 May 2022 13:14:23 |
| Eccentricity: | 0.0029078 |
| inclination: | 97.2667° |
| perigee height: | 437 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 138.5226° |
| argument of perigee: | 231.0972° |
| revolutions per day: | 15.36138687 |
| mean anomaly at epoch: | 128.7679° |
| orbit number at epoch: | 52577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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