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 43806U 18099BA 25138.85500623 .00005540 00000-0 33862-3 0 9995
2 43806 97.4537 191.3167 0006568 245.1652 114.8895 15.10638863352801
| Epoch (UTC): | 18 May 2025 20:31:12 |
| Eccentricity: | 0.0006568 |
| inclination: | 97.4537° |
| perigee height: | 530 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 191.3167° |
| argument of perigee: | 245.1652° |
| revolutions per day: | 15.10638863 |
| mean anomaly at epoch: | 114.8895° |
| orbit number at epoch: | 35280 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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