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 57445U 26145.54863749 +.00000000 +00000-0 +37233-4 0 00004
2 57445 43.0018 186.0275 0001096 277.9818 82.0909 15.27577966 03
| Epoch (UTC): | 25 May 2026 13:10:02 |
| Eccentricity: | 0.0001096 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.0275° |
| argument of perigee: | 277.9818° |
| revolutions per day: | 15.27577966 |
| mean anomaly at epoch: | 82.0909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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