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 61932U 26145.48776339 +.00000000 +00000-0 +51896-3 0 00001
2 61932 43.0035 211.8024 0000591 285.9755 74.1032 15.27584915 06
| Epoch (UTC): | 25 May 2026 11:42:22 |
| Eccentricity: | 0.0000591 |
| inclination: | 43.0035° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 211.8024° |
| argument of perigee: | 285.9755° |
| revolutions per day: | 15.27584915 |
| mean anomaly at epoch: | 74.1032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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