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 41183U 26145.60606852 +.00000000 +00000-0 +16141-3 0 00007
2 41183 47.0035 108.5356 0004045 291.2713 68.7741 14.58857321 01
| Epoch (UTC): | 25 May 2026 14:32:44 |
| Eccentricity: | 0.0004045 |
| inclination: | 47.0035° |
| perigee height: | 694 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 108.5356° |
| argument of perigee: | 291.2713° |
| revolutions per day: | 14.58857321 |
| mean anomaly at epoch: | 68.7741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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