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 46114U 26145.51919816 +.00000000 +00000-0 +00000-0 0 00007
2 46114 0.0162 338.3258 0002274 85.0611 241.6450 1.00273609 05
| Epoch (UTC): | 25 May 2026 12:27:38 |
| Eccentricity: | 0.0002274 |
| inclination: | 0.0162° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 338.3258° |
| argument of perigee: | 85.0611° |
| revolutions per day: | 1.00273609 |
| mean anomaly at epoch: | 241.6450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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