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 63637U 26144.88535882 +.00000000 +00000-0 +84861-3 0 00002
2 63637 43.0015 294.5907 0001754 283.6104 76.4552 15.27615688 05
| Epoch (UTC): | 24 May 2026 21:14:55 |
| Eccentricity: | 0.0001754 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 294.5907° |
| argument of perigee: | 283.6104° |
| revolutions per day: | 15.27615688 |
| mean anomaly at epoch: | 76.4552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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