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 46786U 26145.58335647 +.00000000 +00000-0 +91461-2 0 00006
2 46786 53.0437 251.6534 0001552 68.3892 185.1414 15.64570716 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.0437° |
| perigee height: | 373 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 251.6534° |
| argument of perigee: | 68.3892° |
| revolutions per day: | 15.64570716 |
| mean anomaly at epoch: | 185.1414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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