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 63550U 26145.03847250 +.00000000 +00000-0 +11956-2 0 00003
2 63550 43.0004 53.8349 0001346 231.3227 128.7520 15.70964241 02
| Epoch (UTC): | 25 May 2026 00:55:24 |
| Eccentricity: | 0.0001346 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 53.8349° |
| argument of perigee: | 231.3227° |
| revolutions per day: | 15.70964241 |
| mean anomaly at epoch: | 128.7520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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