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 25341.23849968 .00000735 00000-0 26232-3 0 9991
2 39090 98.3824 161.2709 0009785 85.4298 274.8007 14.36997882669497
| Epoch (UTC): | 07 December 2025 05:43:26 |
| Eccentricity: | 0.0009785 |
| inclination: | 98.3824° |
| perigee height: | 761 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 161.2709° |
| argument of perigee: | 85.4298° |
| revolutions per day: | 14.36997882 |
| mean anomaly at epoch: | 274.8007° |
| orbit number at epoch: | 66949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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