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 63603U 26145.56559977 +.00000000 +00000-0 +78383-4 0 00005
2 63603 99.6895 153.0578 0001198 88.6896 271.4380 13.57239050 09
| Epoch (UTC): | 25 May 2026 13:34:27 |
| Eccentricity: | 0.0001198 |
| inclination: | 99.6895° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.0578° |
| argument of perigee: | 88.6896° |
| revolutions per day: | 13.57239050 |
| mean anomaly at epoch: | 271.4380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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