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 46565U 26145.58335647 +.00000000 +00000-0 +71459-3 0 00007
2 46565 53.0355 98.6054 0010506 69.4496 298.3001 15.77937444 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0010506 |
| inclination: | 53.0355° |
| perigee height: | 329 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 98.6054° |
| argument of perigee: | 69.4496° |
| revolutions per day: | 15.77937444 |
| mean anomaly at epoch: | 298.3001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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