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 40549U 26145.38829728 +.00000000 +00000-0 +00000-0 0 00000
2 40549 49.2385 295.7329 0038014 189.8646 350.4188 1.00254906 06
| Epoch (UTC): | 25 May 2026 09:19:08 |
| Eccentricity: | 0.0038014 |
| inclination: | 49.2385° |
| perigee height: | 35631 km |
| apogee height: | 35952 km |
| right ascension of ascending node: | 295.7329° |
| argument of perigee: | 189.8646° |
| revolutions per day: | 1.00254906 |
| mean anomaly at epoch: | 350.4188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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