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 23086.80373814 .00000691 00000-0 25482-3 0 9997
2 39090 98.3926 282.3821 0009688 141.6536 218.5341 14.35519695528044
| Epoch (UTC): | 27 March 2023 19:17:22 |
| Eccentricity: | 0.0009688 |
| inclination: | 98.3926° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 282.3821° |
| argument of perigee: | 141.6536° |
| revolutions per day: | 14.35519695 |
| mean anomaly at epoch: | 218.5341° |
| orbit number at epoch: | 52804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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