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 63415U 26145.41119708 +.00000000 +00000-0 +42194-3 0 00004
2 63415 43.0067 33.7339 0000965 260.6425 99.4318 15.27596977 06
| Epoch (UTC): | 25 May 2026 09:52:07 |
| Eccentricity: | 0.0000965 |
| inclination: | 43.0067° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7339° |
| argument of perigee: | 260.6425° |
| revolutions per day: | 15.27596977 |
| mean anomaly at epoch: | 99.4318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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