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 63753U 26145.52994172 +.00000000 +00000-0 +83143-3 0 00006
2 63753 43.0001 188.7951 0001463 262.5528 97.5174 15.70859103 09
| Epoch (UTC): | 25 May 2026 12:43:06 |
| Eccentricity: | 0.0001463 |
| inclination: | 43.0001° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 188.7951° |
| argument of perigee: | 262.5528° |
| revolutions per day: | 15.70859103 |
| mean anomaly at epoch: | 97.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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