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 63751U 26145.44524994 +.00000000 +00000-0 +15922-2 0 00005
2 63751 43.0018 189.9018 0001991 273.5661 86.4979 15.70874681 06
| Epoch (UTC): | 25 May 2026 10:41:09 |
| Eccentricity: | 0.0001991 |
| inclination: | 43.0018° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.9018° |
| argument of perigee: | 273.5661° |
| revolutions per day: | 15.70874681 |
| mean anomaly at epoch: | 86.4979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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