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 57156U 26145.48407498 +.00000000 +00000-0 -26553-4 0 00005
2 57156 43.0012 190.0166 0001275 276.2898 83.7808 15.27572367 05
| Epoch (UTC): | 25 May 2026 11:37:04 |
| Eccentricity: | 0.0001275 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.0166° |
| argument of perigee: | 276.2898° |
| revolutions per day: | 15.27572367 |
| mean anomaly at epoch: | 83.7808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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