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 57426U 26145.63519875 +.00000000 +00000-0 +46985-3 0 00004
2 57426 97.2636 210.1239 0013055 87.5044 272.7691 15.28807853 00
| Epoch (UTC): | 25 May 2026 15:14:41 |
| Eccentricity: | 0.0013055 |
| inclination: | 97.2636° |
| perigee height: | 470 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 210.1239° |
| argument of perigee: | 87.5044° |
| revolutions per day: | 15.28807853 |
| mean anomaly at epoch: | 272.7691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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