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 53536U 26145.21047059 +.00000000 +00000-0 -43769-4 0 00005
2 53536 53.2167 80.5255 0001454 81.2385 278.8772 15.08827308 07
| Epoch (UTC): | 25 May 2026 05:03:04 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.2167° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.5255° |
| argument of perigee: | 81.2385° |
| revolutions per day: | 15.08827308 |
| mean anomaly at epoch: | 278.8772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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