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 52606U 26144.82820661 +.00000000 +00000-0 -22158-4 0 00005
2 52606 53.2151 297.3217 0001369 90.0173 270.0976 15.08841014 01
| Epoch (UTC): | 24 May 2026 19:52:37 |
| Eccentricity: | 0.0001369 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 297.3217° |
| argument of perigee: | 90.0173° |
| revolutions per day: | 15.08841014 |
| mean anomaly at epoch: | 270.0976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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