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 26071.15917148 +.00000000 +00000-0 +17667-3 0 00005
2 25544 51.6325 60.1463 0007984 183.4136 176.6799 15.48595269 07
| Epoch (UTC): | 12 March 2026 03:49:12 |
| Eccentricity: | 0.0007984 |
| inclination: | 51.6325° |
| perigee height: | 415 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 60.1463° |
| argument of perigee: | 183.4136° |
| revolutions per day: | 15.48595269 |
| mean anomaly at epoch: | 176.6799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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