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 63655U 26144.79314172 +.00000000 +00000-0 +10339-2 0 00007
2 63655 43.0019 295.6092 0001277 275.6405 84.4301 15.27607181 01
| Epoch (UTC): | 24 May 2026 19:02:07 |
| Eccentricity: | 0.0001277 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.6092° |
| argument of perigee: | 275.6405° |
| revolutions per day: | 15.27607181 |
| mean anomaly at epoch: | 84.4301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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