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 56550U 26145.48524167 +.00000000 +00000-0 +12183-4 0 00008
2 56550 43.0035 150.1701 0001644 272.2403 87.8260 15.27576238 05
| Epoch (UTC): | 25 May 2026 11:38:44 |
| Eccentricity: | 0.0001644 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1701° |
| argument of perigee: | 272.2403° |
| revolutions per day: | 15.27576238 |
| mean anomaly at epoch: | 87.8260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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