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 59936U 26145.02417274 +.00000000 +00000-0 +15545-3 0 00003
2 59936 43.0006 261.7274 0001021 282.8770 77.1968 15.27562260 08
| Epoch (UTC): | 25 May 2026 00:34:48 |
| Eccentricity: | 0.0001021 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.7274° |
| argument of perigee: | 282.8770° |
| revolutions per day: | 15.27562260 |
| mean anomaly at epoch: | 77.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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