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 62817U 26145.18925007 +.00000000 +00000-0 +70504-3 0 00006
2 62817 53.1600 314.0616 0001186 83.2738 276.8398 15.30207208 00
| Epoch (UTC): | 25 May 2026 04:32:31 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0616° |
| argument of perigee: | 83.2738° |
| revolutions per day: | 15.30207208 |
| mean anomaly at epoch: | 276.8398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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