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 55621U 26144.80980102 +.00000000 +00000-0 -13259-4 0 00002
2 55621 43.0019 284.1046 0001570 274.0469 86.0203 15.27574630 07
| Epoch (UTC): | 24 May 2026 19:26:06 |
| Eccentricity: | 0.0001570 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.1046° |
| argument of perigee: | 274.0469° |
| revolutions per day: | 15.27574630 |
| mean anomaly at epoch: | 86.0203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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