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 53911U 26145.53709073 +.00000000 +00000-0 +28851-4 0 00002
2 53911 53.2132 329.3170 0001388 91.1804 268.9348 15.08838276 03
| Epoch (UTC): | 25 May 2026 12:53:24 |
| Eccentricity: | 0.0001388 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.3170° |
| argument of perigee: | 91.1804° |
| revolutions per day: | 15.08838276 |
| mean anomaly at epoch: | 268.9348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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