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 22141.52954664 .00000367 00000-0 14285-3 0 9994
2 39090 98.4062 340.3676 0009060 359.8212 0.2969 14.35289132483533
| Epoch (UTC): | 21 May 2022 12:42:32 |
| Eccentricity: | 0.0009060 |
| inclination: | 98.4062° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 340.3676° |
| argument of perigee: | 359.8212° |
| revolutions per day: | 14.35289132 |
| mean anomaly at epoch: | 0.2969° |
| orbit number at epoch: | 48353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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