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 63196U 26145.04300579 +.00000000 +00000-0 +61175-3 0 00007
2 63196 43.0032 18.1233 0001897 263.6224 96.4412 15.27619536 08
| Epoch (UTC): | 25 May 2026 01:01:55 |
| Eccentricity: | 0.0001897 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 18.1233° |
| argument of perigee: | 263.6224° |
| revolutions per day: | 15.27619536 |
| mean anomaly at epoch: | 96.4412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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