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 39090U 13009E 22175.54917993 .00000126 00000-0 58790-4 0 9990
2 39090 98.4043 13.5007 0007862 247.7768 112.2584 14.35296062488417
| Epoch (UTC): | 24 June 2022 13:10:49 |
| Eccentricity: | 0.0007862 |
| inclination: | 98.4043° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 13.5007° |
| argument of perigee: | 247.7768° |
| revolutions per day: | 14.35296062 |
| mean anomaly at epoch: | 112.2584° |
| orbit number at epoch: | 48841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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