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 23086.10672334 .00000735 00000-0 27023-3 0 9991
2 39090 98.3926 281.7039 0009650 143.5834 216.6010 14.35518836527967
| Epoch (UTC): | 27 March 2023 02:33:40 |
| Eccentricity: | 0.0009650 |
| inclination: | 98.3926° |
| perigee height: | 766 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 281.7039° |
| argument of perigee: | 143.5834° |
| revolutions per day: | 14.35518836 |
| mean anomaly at epoch: | 216.6010° |
| orbit number at epoch: | 52796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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