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 58650U 26140.70091955 +.00000000 +00000-0 +10397-3 0 00009
2 58650 97.4041 109.8851 0002037 277.5903 82.5089 14.98082859 04
| Epoch (UTC): | 20 May 2026 16:49:19 |
| Eccentricity: | 0.0002037 |
| inclination: | 97.4041° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 109.8851° |
| argument of perigee: | 277.5903° |
| revolutions per day: | 14.98082859 |
| mean anomaly at epoch: | 82.5089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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