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 57753U 26145.28162697 +.00000000 +00000-0 +52624-4 0 00002
2 57753 43.0051 107.2670 0001372 275.4709 84.5986 15.27580189 08
| Epoch (UTC): | 25 May 2026 06:45:32 |
| Eccentricity: | 0.0001372 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.2670° |
| argument of perigee: | 275.4709° |
| revolutions per day: | 15.27580189 |
| mean anomaly at epoch: | 84.5986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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