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 43587U 26145.60511279 +.00000000 +00000-0 +00000-0 0 00009
2 43587 0.0159 300.6724 0001581 143.9095 124.4522 1.00268808 05
| Epoch (UTC): | 25 May 2026 14:31:21 |
| Eccentricity: | 0.0001581 |
| inclination: | 0.0159° |
| perigee height: | 35781 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 300.6724° |
| argument of perigee: | 143.9095° |
| revolutions per day: | 1.00268808 |
| mean anomaly at epoch: | 124.4522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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