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 41185U 26145.38149968 +.00000000 +00000-0 +11215-3 0 00001
2 41185 47.0022 18.4505 0001016 103.7928 256.3071 14.58828501 03
| Epoch (UTC): | 25 May 2026 09:09:21 |
| Eccentricity: | 0.0001016 |
| inclination: | 47.0022° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 18.4505° |
| argument of perigee: | 103.7928° |
| revolutions per day: | 14.58828501 |
| mean anomaly at epoch: | 256.3071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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