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 57175U 26145.60350213 +.00000000 +00000-0 +42664-3 0 00001
2 57175 97.5064 208.6275 0010107 185.8467 174.2656 15.28530512 09
| Epoch (UTC): | 25 May 2026 14:29:02 |
| Eccentricity: | 0.0010107 |
| inclination: | 97.5064° |
| perigee height: | 473 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 208.6275° |
| argument of perigee: | 185.8467° |
| revolutions per day: | 15.28530512 |
| mean anomaly at epoch: | 174.2656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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