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 53891U 26145.66668980 +.00000000 +00000-0 +17173-2 0 00007
2 53891 53.2176 333.5331 0001348 82.3115 61.0533 15.34525005 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.2176° |
| perigee height: | 461 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 333.5331° |
| argument of perigee: | 82.3115° |
| revolutions per day: | 15.34525005 |
| mean anomaly at epoch: | 61.0533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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