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 63837U 26145.33919404 +.00000000 +00000-0 +51876-3 0 00001
2 63837 43.0019 5.1200 0001846 250.8638 109.2014 15.27589756 07
| Epoch (UTC): | 25 May 2026 08:08:26 |
| Eccentricity: | 0.0001846 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.1200° |
| argument of perigee: | 250.8638° |
| revolutions per day: | 15.27589756 |
| mean anomaly at epoch: | 109.2014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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