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 41942U 26145.43402676 +.00000000 +00000-0 +00000-0 0 00003
2 41942 0.0020 227.5236 0001013 197.2725 298.4838 1.00274474 00
| Epoch (UTC): | 25 May 2026 10:24:59 |
| Eccentricity: | 0.0001013 |
| inclination: | 0.0020° |
| perigee height: | 35782 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 227.5236° |
| argument of perigee: | 197.2725° |
| revolutions per day: | 1.00274474 |
| mean anomaly at epoch: | 298.4838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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