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 57171U 26145.59928608 +.00000000 +00000-0 +34852-3 0 00004
2 57171 97.5127 207.1241 0011147 182.1647 177.9543 15.23748758 00
| Epoch (UTC): | 25 May 2026 14:22:58 |
| Eccentricity: | 0.0011147 |
| inclination: | 97.5127° |
| perigee height: | 487 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 207.1241° |
| argument of perigee: | 182.1647° |
| revolutions per day: | 15.23748758 |
| mean anomaly at epoch: | 177.9543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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