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 62926U 26145.47389229 +.00000000 +00000-0 +72749-3 0 00002
2 62926 43.0068 55.3893 0002111 282.1218 77.9397 15.27600624 05
| Epoch (UTC): | 25 May 2026 11:22:24 |
| Eccentricity: | 0.0002111 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.3893° |
| argument of perigee: | 282.1218° |
| revolutions per day: | 15.27600624 |
| mean anomaly at epoch: | 77.9397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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