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 25544U 26112.52244764 +.00000000 +00000-0 +14744-3 0 00002
2 25544 51.6320 215.6072 0006766 337.8366 22.2329 15.48891662 03
| Epoch (UTC): | 22 April 2026 12:32:19 |
| Eccentricity: | 0.0006766 |
| inclination: | 51.6320° |
| perigee height: | 415 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 215.6072° |
| argument of perigee: | 337.8366° |
| revolutions per day: | 15.48891662 |
| mean anomaly at epoch: | 22.2329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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