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 23337.77560182 .00000724 00000-0 26478-3 0 9991
2 39090 98.3803 166.4773 0009866 115.6537 244.5669 14.35800304564071
| Epoch (UTC): | 03 December 2023 18:36:51 |
| Eccentricity: | 0.0009866 |
| inclination: | 98.3803° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 166.4773° |
| argument of perigee: | 115.6537° |
| revolutions per day: | 14.35800304 |
| mean anomaly at epoch: | 244.5669° |
| orbit number at epoch: | 56407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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