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 57109U 26145.23310084 +.00000000 +00000-0 +34379-4 0 00004
2 57109 43.0032 209.7099 0002081 285.1785 74.8837 15.27576881 06
| Epoch (UTC): | 25 May 2026 05:35:39 |
| Eccentricity: | 0.0002081 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.7099° |
| argument of perigee: | 285.1785° |
| revolutions per day: | 15.27576881 |
| mean anomaly at epoch: | 74.8837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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