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 63757U 26145.26499752 +.00000000 +00000-0 +14169-2 0 00006
2 63757 43.0004 190.2409 0001683 238.8152 121.2551 15.70953299 00
| Epoch (UTC): | 25 May 2026 06:21:35 |
| Eccentricity: | 0.0001683 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 190.2409° |
| argument of perigee: | 238.8152° |
| revolutions per day: | 15.70953299 |
| mean anomaly at epoch: | 121.2551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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