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 23090.49790746 .00000800 00000-0 29253-3 0 9996
2 39090 98.3925 285.9765 0009850 131.5032 228.7001 14.35525926528599
| Epoch (UTC): | 31 March 2023 11:56:59 |
| Eccentricity: | 0.0009850 |
| inclination: | 98.3925° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 285.9765° |
| argument of perigee: | 131.5032° |
| revolutions per day: | 14.35525926 |
| mean anomaly at epoch: | 228.7001° |
| orbit number at epoch: | 52859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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