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 57708U 26145.12902512 +.00000000 +00000-0 -50748-4 0 00009
2 57708 43.0037 46.1597 0001581 255.1116 104.9561 15.27597607 09
| Epoch (UTC): | 25 May 2026 03:05:47 |
| Eccentricity: | 0.0001581 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.1597° |
| argument of perigee: | 255.1116° |
| revolutions per day: | 15.27597607 |
| mean anomaly at epoch: | 104.9561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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