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 57704U 26145.11491198 +.00000000 +00000-0 +21289-4 0 00004
2 57704 43.0073 46.0583 0001801 265.7266 94.3380 15.27591041 04
| Epoch (UTC): | 25 May 2026 02:45:28 |
| Eccentricity: | 0.0001801 |
| inclination: | 43.0073° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.0583° |
| argument of perigee: | 265.7266° |
| revolutions per day: | 15.27591041 |
| mean anomaly at epoch: | 94.3380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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