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 63110U 26145.29521001 +.00000000 +00000-0 +16799-2 0 00006
2 63110 43.0006 135.0810 0001815 271.4910 88.5749 15.70875625 00
| Epoch (UTC): | 25 May 2026 07:05:06 |
| Eccentricity: | 0.0001815 |
| inclination: | 43.0006° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 135.0810° |
| argument of perigee: | 271.4910° |
| revolutions per day: | 15.70875625 |
| mean anomaly at epoch: | 88.5749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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