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 55599U 26145.10475071 +.00000000 +00000-0 -20157-4 0 00009
2 55599 43.0055 282.8651 0001917 273.8405 86.2227 15.27570774 03
| Epoch (UTC): | 25 May 2026 02:30:50 |
| Eccentricity: | 0.0001917 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 282.8651° |
| argument of perigee: | 273.8405° |
| revolutions per day: | 15.27570774 |
| mean anomaly at epoch: | 86.2227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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