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 58908U 26145.59369105 +.00000000 +00000-0 +20430-3 0 00001
2 58908 49.9926 70.2094 0006450 311.9627 48.0767 14.97050965 05
| Epoch (UTC): | 25 May 2026 14:14:54 |
| Eccentricity: | 0.0006450 |
| inclination: | 49.9926° |
| perigee height: | 572 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 70.2094° |
| argument of perigee: | 311.9627° |
| revolutions per day: | 14.97050965 |
| mean anomaly at epoch: | 48.0767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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