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 59349U 26145.13191985 +.00000000 +00000-0 +89850-4 0 00002
2 59349 43.0018 188.1556 0001362 269.0289 91.0406 15.27573810 09
| Epoch (UTC): | 25 May 2026 03:09:57 |
| Eccentricity: | 0.0001362 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.1556° |
| argument of perigee: | 269.0289° |
| revolutions per day: | 15.27573810 |
| mean anomaly at epoch: | 91.0406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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