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 23081.50641271 .00000625 00000-0 23204-3 0 9991
2 39090 98.3928 277.2276 0009390 156.5940 203.5676 14.35510902527302
| Epoch (UTC): | 22 March 2023 12:09:14 |
| Eccentricity: | 0.0009390 |
| inclination: | 98.3928° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 277.2276° |
| argument of perigee: | 156.5940° |
| revolutions per day: | 14.35510902 |
| mean anomaly at epoch: | 203.5676° |
| orbit number at epoch: | 52730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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