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 22270.77501428 .00000186 00000-0 79770-4 0 9990
2 39090 98.3998 106.2259 0008538 333.8642 26.2112 14.35330953502071
| Epoch (UTC): | 27 September 2022 18:36:01 |
| Eccentricity: | 0.0008538 |
| inclination: | 98.3998° |
| perigee height: | 768 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 106.2259° |
| argument of perigee: | 333.8642° |
| revolutions per day: | 14.35330953 |
| mean anomaly at epoch: | 26.2112° |
| orbit number at epoch: | 50207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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