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 43572U 26145.33484280 +.00000000 +00000-0 +74038-5 0 00001
2 43572 86.3969 66.3570 0002122 82.2362 277.9075 14.34217961 06
| Epoch (UTC): | 25 May 2026 08:02:10 |
| Eccentricity: | 0.0002122 |
| inclination: | 86.3969° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.3570° |
| argument of perigee: | 82.2362° |
| revolutions per day: | 14.34217961 |
| mean anomaly at epoch: | 277.9075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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