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 23078.78803563 .00000637 00000-0 23605-3 0 9999
2 39090 98.3929 274.5825 0009230 164.3773 195.7699 14.35507099526890
| Epoch (UTC): | 19 March 2023 18:54:46 |
| Eccentricity: | 0.0009230 |
| inclination: | 98.3929° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 274.5825° |
| argument of perigee: | 164.3773° |
| revolutions per day: | 14.35507099 |
| mean anomaly at epoch: | 195.7699° |
| orbit number at epoch: | 52689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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