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 41191U 26145.59092181 +.00000000 +00000-0 +00000-0 0 00002
2 41191 0.0178 328.2291 0003052 93.4386 70.3315 1.00270314 01
| Epoch (UTC): | 25 May 2026 14:10:55 |
| Eccentricity: | 0.0003052 |
| inclination: | 0.0178° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 328.2291° |
| argument of perigee: | 93.4386° |
| revolutions per day: | 1.00270314 |
| mean anomaly at epoch: | 70.3315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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