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 26106.19926477 +.00000000 +00000-0 +10584-3 0 00004
2 25544 51.6325 246.8823 0006616 318.5233 41.5253 15.48930915 06
| Epoch (UTC): | 16 April 2026 04:46:56 |
| Eccentricity: | 0.0006616 |
| inclination: | 51.6325° |
| perigee height: | 415 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 246.8823° |
| argument of perigee: | 318.5233° |
| revolutions per day: | 15.48930915 |
| mean anomaly at epoch: | 41.5253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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