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 41238U 26145.59395514 +.00000000 +00000-0 +00000-0 0 00000
2 41238 0.0198 209.6629 0002206 180.1362 118.6803 1.00273647 00
| Epoch (UTC): | 25 May 2026 14:15:17 |
| Eccentricity: | 0.0002206 |
| inclination: | 0.0198° |
| perigee height: | 35777 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 209.6629° |
| argument of perigee: | 180.1362° |
| revolutions per day: | 1.00273647 |
| mean anomaly at epoch: | 118.6803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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