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 41184U 26145.33703696 +.00000000 +00000-0 +17106-3 0 00004
2 41184 47.0007 18.2953 0002458 101.7171 258.3991 14.58864514 06
| Epoch (UTC): | 25 May 2026 08:05:19 |
| Eccentricity: | 0.0002458 |
| inclination: | 47.0007° |
| perigee height: | 695 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 18.2953° |
| argument of perigee: | 101.7171° |
| revolutions per day: | 14.58864514 |
| mean anomaly at epoch: | 258.3991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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