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 43577U 26145.49341426 +.00000000 +00000-0 +74302-4 0 00000
2 43577 86.3969 66.2566 0002057 84.6214 275.5216 14.34219964 00
| Epoch (UTC): | 25 May 2026 11:50:30 |
| Eccentricity: | 0.0002057 |
| inclination: | 86.3969° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2566° |
| argument of perigee: | 84.6214° |
| revolutions per day: | 14.34219964 |
| mean anomaly at epoch: | 275.5216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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