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 56888U 26145.35704269 +.00000000 +00000-0 +33884-4 0 00002
2 56888 43.0058 15.8045 0001259 270.5077 89.5630 15.27579445 05
| Epoch (UTC): | 25 May 2026 08:34:08 |
| Eccentricity: | 0.0001259 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 15.8045° |
| argument of perigee: | 270.5077° |
| revolutions per day: | 15.27579445 |
| mean anomaly at epoch: | 89.5630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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