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 19751U 26145.48140596 +.00000000 +00000-0 +00000-0 0 00001
2 19751 64.9332 72.9716 0023326 217.6042 323.8591 2.13155987 04
| Epoch (UTC): | 25 May 2026 11:33:13 |
| Eccentricity: | 0.0023326 |
| inclination: | 64.9332° |
| perigee height: | 19066 km |
| apogee height: | 19185 km |
| right ascension of ascending node: | 72.9716° |
| argument of perigee: | 217.6042° |
| revolutions per day: | 2.13155987 |
| mean anomaly at epoch: | 323.8591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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