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 57456U 26145.59462551 +.00000000 +00000-0 +24003-3 0 00007
2 57456 34.9927 221.2807 0008808 149.9986 210.1233 15.18084993 05
| Epoch (UTC): | 25 May 2026 14:16:15 |
| Eccentricity: | 0.0008808 |
| inclination: | 34.9927° |
| perigee height: | 506 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 221.2807° |
| argument of perigee: | 149.9986° |
| revolutions per day: | 15.18084993 |
| mean anomaly at epoch: | 210.1233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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