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 44113U 26145.45152005 +.00000000 +00000-0 +00000-0 0 00006
2 44113 0.0663 341.8878 0003991 67.5893 310.5573 5.00116159 01
| Epoch (UTC): | 25 May 2026 10:50:11 |
| Eccentricity: | 0.0003991 |
| inclination: | 0.0663° |
| perigee height: | 8060 km |
| apogee height: | 8072 km |
| right ascension of ascending node: | 341.8878° |
| argument of perigee: | 67.5893° |
| revolutions per day: | 5.00116159 |
| mean anomaly at epoch: | 310.5573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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