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 57817U 26145.44536527 +.00000000 +00000-0 +65962-3 0 00006
2 57817 43.0013 161.0001 0001933 261.6865 98.3768 15.27591857 01
| Epoch (UTC): | 25 May 2026 10:41:19 |
| Eccentricity: | 0.0001933 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.0001° |
| argument of perigee: | 261.6865° |
| revolutions per day: | 15.27591857 |
| mean anomaly at epoch: | 98.3768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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