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 58073U 26145.59451536 +.00000000 +00000-0 +12503-3 0 00006
2 58073 98.4986 171.7704 0000301 128.2931 231.8280 14.32713416 02
| Epoch (UTC): | 25 May 2026 14:16:06 |
| Eccentricity: | 0.0000301 |
| inclination: | 98.4986° |
| perigee height: | 782 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 171.7704° |
| argument of perigee: | 128.2931° |
| revolutions per day: | 14.32713416 |
| mean anomaly at epoch: | 231.8280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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