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 is defined by the following mean orbital elements,
1 43476U 18047A 26108.12268517 +.00002542 00000-0 +68217-4 0 07
2 43476 88.9953 206.1984 0009817 1.1145 84.2729 15.37840307440575
| Epoch (UTC): | 18 April 2026 02:56:39 |
| Eccentricity: | 0.0009817 |
| inclination: | 88.9953° |
| perigee height: | 446 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 206.1984° |
| argument of perigee: | 1.1145° |
| revolutions per day: | 15.37840307 |
| mean anomaly at epoch: | 84.2729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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