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 57715U 26145.13674808 +.00000000 +00000-0 -17397-4 0 00005
2 57715 43.0022 46.2146 0001037 245.4844 114.5900 15.27596399 09
| Epoch (UTC): | 25 May 2026 03:16:55 |
| Eccentricity: | 0.0001037 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.2146° |
| argument of perigee: | 245.4844° |
| revolutions per day: | 15.27596399 |
| mean anomaly at epoch: | 114.5900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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