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 41911U 26145.52562509 +.00000000 +00000-0 +00000-0 0 00001
2 41911 0.7769 85.6054 0000553 337.3107 75.9603 1.00270425 03
| Epoch (UTC): | 25 May 2026 12:36:54 |
| Eccentricity: | 0.0000553 |
| inclination: | 0.7769° |
| perigee height: | 35785 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 85.6054° |
| argument of perigee: | 337.3107° |
| revolutions per day: | 1.00270425 |
| mean anomaly at epoch: | 75.9603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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