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 43611U 26145.53982602 +.00000000 +00000-0 +00000-0 0 00001
2 43611 0.0141 285.5173 0001983 128.1279 161.8089 1.00273678 02
| Epoch (UTC): | 25 May 2026 12:57:20 |
| Eccentricity: | 0.0001983 |
| inclination: | 0.0141° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 285.5173° |
| argument of perigee: | 128.1279° |
| revolutions per day: | 1.00273678 |
| mean anomaly at epoch: | 161.8089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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