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 00658U 26130.66430809 +.00000000 +00000-0 +96417-3 0 00000
2 00658 65.8637 221.0952 0359055 233.0994 123.6653 13.41755157 09
| Epoch (UTC): | 10 May 2026 15:56:36 |
| Eccentricity: | 0.0359055 |
| inclination: | 65.8637° |
| perigee height: | 834 km |
| apogee height: | 1371 km |
| right ascension of ascending node: | 221.0952° |
| argument of perigee: | 233.0994° |
| revolutions per day: | 13.41755157 |
| mean anomaly at epoch: | 123.6653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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