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 59092U 26145.56538316 +.00000000 +00000-0 +33561-4 0 00005
2 59092 43.0025 236.9784 0000835 282.4481 77.6277 15.27582427 04
| Epoch (UTC): | 25 May 2026 13:34:09 |
| Eccentricity: | 0.0000835 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.9784° |
| argument of perigee: | 282.4481° |
| revolutions per day: | 15.27582427 |
| mean anomaly at epoch: | 77.6277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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