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 41904U 26145.31836395 +.00000000 +00000-0 +00000-0 0 00007
2 41904 0.0184 58.3027 0002052 15.4079 199.8061 1.00269634 08
| Epoch (UTC): | 25 May 2026 07:38:26 |
| Eccentricity: | 0.0002052 |
| inclination: | 0.0184° |
| perigee height: | 35779 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 58.3027° |
| argument of perigee: | 15.4079° |
| revolutions per day: | 1.00269634 |
| mean anomaly at epoch: | 199.8061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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