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 59923U 26145.33568838 +.00000000 +00000-0 +50766-4 0 00001
2 59923 43.0008 259.7695 0001421 275.0155 85.0534 15.27573696 07
| Epoch (UTC): | 25 May 2026 08:03:23 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.7695° |
| argument of perigee: | 275.0155° |
| revolutions per day: | 15.27573696 |
| mean anomaly at epoch: | 85.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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