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 53574U 26145.49103757 +.00000000 +00000-0 +16568-4 0 00001
2 53574 53.2126 69.0562 0001396 84.3574 275.7577 15.08833004 05
| Epoch (UTC): | 25 May 2026 11:47:05 |
| Eccentricity: | 0.0001396 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.0562° |
| argument of perigee: | 84.3574° |
| revolutions per day: | 15.08833004 |
| mean anomaly at epoch: | 275.7577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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