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 56133U 26145.52155446 +.00000000 +00000-0 +34185-4 0 00006
2 56133 43.0062 72.8188 0001695 274.8866 85.1792 15.27567230 01
| Epoch (UTC): | 25 May 2026 12:31:02 |
| Eccentricity: | 0.0001695 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 72.8188° |
| argument of perigee: | 274.8866° |
| revolutions per day: | 15.27567230 |
| mean anomaly at epoch: | 85.1792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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