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 26084.45430866 +.00000000 +00000-0 +24673-3 0 00004
2 25544 51.6344 354.4276 0006215 231.1671 128.8763 15.48531543 05
| Epoch (UTC): | 25 March 2026 10:54:12 |
| Eccentricity: | 0.0006215 |
| inclination: | 51.6344° |
| perigee height: | 417 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 354.4276° |
| argument of perigee: | 231.1671° |
| revolutions per day: | 15.48531543 |
| mean anomaly at epoch: | 128.8763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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