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 59850U 26145.55830137 +.00000000 +00000-0 +29549-4 0 00003
2 59850 43.0004 200.1782 0001491 263.2919 96.7763 15.27576617 02
| Epoch (UTC): | 25 May 2026 13:23:57 |
| Eccentricity: | 0.0001491 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.1782° |
| argument of perigee: | 263.2919° |
| revolutions per day: | 15.27576617 |
| mean anomaly at epoch: | 96.7763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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