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 24340.51365230 .00001081 00000-0 38273-3 0 9998
2 39090 98.3768 164.1438 0009856 99.4846 260.7455 14.36499832616831
| Epoch (UTC): | 05 December 2024 12:19:39 |
| Eccentricity: | 0.0009856 |
| inclination: | 98.3768° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 164.1438° |
| argument of perigee: | 99.4846° |
| revolutions per day: | 14.36499832 |
| mean anomaly at epoch: | 260.7455° |
| orbit number at epoch: | 61683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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