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 59937U 26145.36138429 +.00000000 +00000-0 +25612-4 0 00000
2 59937 43.0018 259.9585 0001149 274.3233 85.7487 15.27577188 03
| Epoch (UTC): | 25 May 2026 08:40:23 |
| Eccentricity: | 0.0001149 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.9585° |
| argument of perigee: | 274.3233° |
| revolutions per day: | 15.27577188 |
| mean anomaly at epoch: | 85.7487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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