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 41945U 26145.20331358 +.00000000 +00000-0 +00000-0 0 00009
2 41945 0.0176 331.4767 0000275 344.3089 317.0214 1.00270562 06
| Epoch (UTC): | 25 May 2026 04:52:46 |
| Eccentricity: | 0.0000275 |
| inclination: | 0.0176° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 331.4767° |
| argument of perigee: | 344.3089° |
| revolutions per day: | 1.00270562 |
| mean anomaly at epoch: | 317.0214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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