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 58545U 26145.16566001 +.00000000 +00000-0 +85855-4 0 00008
2 58545 53.1604 66.8483 0001455 99.8828 260.2339 15.34398003 03
| Epoch (UTC): | 25 May 2026 03:58:33 |
| Eccentricity: | 0.0001455 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 66.8483° |
| argument of perigee: | 99.8828° |
| revolutions per day: | 15.34398003 |
| mean anomaly at epoch: | 260.2339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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