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 23341.46905106 .00000364 00000-0 14053-3 0 9997
2 39090 98.3801 170.0681 0009948 105.5320 254.6966 14.35803669564582
| Epoch (UTC): | 07 December 2023 11:15:26 |
| Eccentricity: | 0.0009948 |
| inclination: | 98.3801° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 170.0681° |
| argument of perigee: | 105.5320° |
| revolutions per day: | 14.35803669 |
| mean anomaly at epoch: | 254.6966° |
| orbit number at epoch: | 56458 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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