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 59927U 26145.04587056 +.00000000 +00000-0 -18868-4 0 00004
2 59927 43.0037 261.0374 0001466 275.0450 85.0234 15.27575499 00
| Epoch (UTC): | 25 May 2026 01:06:03 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.0374° |
| argument of perigee: | 275.0450° |
| revolutions per day: | 15.27575499 |
| mean anomaly at epoch: | 85.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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