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 55591U 26144.87902176 +.00000000 +00000-0 +10202-3 0 00003
2 55591 43.0050 295.0408 0001570 280.3878 79.6797 15.27577391 08
| Epoch (UTC): | 24 May 2026 21:05:47 |
| Eccentricity: | 0.0001570 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.0408° |
| argument of perigee: | 280.3878° |
| revolutions per day: | 15.27577391 |
| mean anomaly at epoch: | 79.6797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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