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 43805U 18099AZ 25138.68414635 .00028395 00000-0 90879-3 0 9996
2 43805 97.4556 202.6513 0007748 185.0704 175.0461 15.32338587353828
| Epoch (UTC): | 18 May 2025 16:25:10 |
| Eccentricity: | 0.0007748 |
| inclination: | 97.4556° |
| perigee height: | 463 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 202.6513° |
| argument of perigee: | 185.0704° |
| revolutions per day: | 15.32338587 |
| mean anomaly at epoch: | 175.0461° |
| orbit number at epoch: | 35382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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