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 26088.13267411 +.00000000 +00000-0 +23326-3 0 00001
2 25544 51.6344 336.2407 0006215 245.2164 114.8178 15.48624340 05
| Epoch (UTC): | 29 March 2026 03:11:03 |
| Eccentricity: | 0.0006215 |
| inclination: | 51.6344° |
| perigee height: | 417 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 336.2407° |
| argument of perigee: | 245.2164° |
| revolutions per day: | 15.48624340 |
| mean anomaly at epoch: | 114.8178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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