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 63737U 26145.63372531 +.00000000 +00000-0 +23874-3 0 00004
2 63737 51.9001 125.3007 0000735 68.2180 291.8861 14.79927746 03
| Epoch (UTC): | 25 May 2026 15:12:33 |
| Eccentricity: | 0.0000735 |
| inclination: | 51.9001° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 125.3007° |
| argument of perigee: | 68.2180° |
| revolutions per day: | 14.79927746 |
| mean anomaly at epoch: | 291.8861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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