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 59654U 26145.50911612 +.00000000 +00000-0 +49203-4 0 00007
2 59654 43.0024 327.7984 0001492 271.3328 88.7353 15.27576775 02
| Epoch (UTC): | 25 May 2026 12:13:07 |
| Eccentricity: | 0.0001492 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.7984° |
| argument of perigee: | 271.3328° |
| revolutions per day: | 15.27576775 |
| mean anomaly at epoch: | 88.7353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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