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 23265.78543811 .00000569 00000-0 21159-3 0 9990
2 39090 98.3868 96.4696 0008553 341.0665 19.0201 14.35693929553727
| Epoch (UTC): | 22 September 2023 18:51:01 |
| Eccentricity: | 0.0008553 |
| inclination: | 98.3868° |
| perigee height: | 766 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 96.4696° |
| argument of perigee: | 341.0665° |
| revolutions per day: | 14.35693929 |
| mean anomaly at epoch: | 19.0201° |
| orbit number at epoch: | 55372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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