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 57126U 26145.23181310 +.00000000 +00000-0 +17001-4 0 00004
2 57126 43.0006 209.6917 0001518 300.4108 59.6593 15.27578967 05
| Epoch (UTC): | 25 May 2026 05:33:48 |
| Eccentricity: | 0.0001518 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.6917° |
| argument of perigee: | 300.4108° |
| revolutions per day: | 15.27578967 |
| mean anomaly at epoch: | 59.6593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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