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 62837U 26145.44292594 +.00000000 +00000-0 +15380-2 0 00005
2 62837 43.0012 203.1913 0003253 259.8234 100.2267 15.70920096 00
| Epoch (UTC): | 25 May 2026 10:37:48 |
| Eccentricity: | 0.0003253 |
| inclination: | 43.0012° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 203.1913° |
| argument of perigee: | 259.8234° |
| revolutions per day: | 15.70920096 |
| mean anomaly at epoch: | 100.2267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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