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 40349U 26145.38452234 +.00000000 +00000-0 +00000-0 0 00002
2 40349 0.0567 356.9117 0002808 50.7062 312.4055 5.00115562 05
| Epoch (UTC): | 25 May 2026 09:13:42 |
| Eccentricity: | 0.0002808 |
| inclination: | 0.0567° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 356.9117° |
| argument of perigee: | 50.7062° |
| revolutions per day: | 5.00115562 |
| mean anomaly at epoch: | 312.4055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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