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 46082U 26145.58335647 +.00000000 +00000-0 -43839-3 0 00003
2 46082 53.1585 104.0198 0001418 86.6499 42.0299 15.31716388 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001418 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.0198° |
| argument of perigee: | 86.6499° |
| revolutions per day: | 15.31716388 |
| mean anomaly at epoch: | 42.0299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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