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 25133.44652405 .00000353 00000-0 13390-3 0 9998
2 39090 98.3826 318.8557 0008483 354.3519 5.7571 14.36797798639654
| Epoch (UTC): | 13 May 2025 10:42:59 |
| Eccentricity: | 0.0008483 |
| inclination: | 98.3826° |
| perigee height: | 763 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 318.8557° |
| argument of perigee: | 354.3519° |
| revolutions per day: | 14.36797798 |
| mean anomaly at epoch: | 5.7571° |
| orbit number at epoch: | 63965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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