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 57498U 26145.49043499 +.00000000 +00000-0 +27823-4 0 00002
2 57498 43.0064 302.1055 0002031 265.4374 94.6246 15.27577079 06
| Epoch (UTC): | 25 May 2026 11:46:13 |
| Eccentricity: | 0.0002031 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.1055° |
| argument of perigee: | 265.4374° |
| revolutions per day: | 15.27577079 |
| mean anomaly at epoch: | 94.6246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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