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 22177.50112264 .00000119 00000-0 56361-4 0 9990
2 39090 98.4040 15.4015 0007914 241.0736 118.9656 14.35296759488690
| Epoch (UTC): | 26 June 2022 12:01:36 |
| Eccentricity: | 0.0007914 |
| inclination: | 98.4040° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 15.4015° |
| argument of perigee: | 241.0736° |
| revolutions per day: | 14.35296759 |
| mean anomaly at epoch: | 118.9656° |
| orbit number at epoch: | 48869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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