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 59252U 26145.05720527 +.00000000 +00000-0 +55713-4 0 00007
2 59252 43.0042 57.6944 0001480 273.8850 86.1832 15.27584346 02
| Epoch (UTC): | 25 May 2026 01:22:22 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.6944° |
| argument of perigee: | 273.8850° |
| revolutions per day: | 15.27584346 |
| mean anomaly at epoch: | 86.1832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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