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 58473U 26144.98927911 +.00000000 +00000-0 +81455-4 0 00000
2 58473 43.0036 356.2998 0001890 273.5647 86.4988 15.27559137 07
| Epoch (UTC): | 24 May 2026 23:44:33 |
| Eccentricity: | 0.0001890 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2998° |
| argument of perigee: | 273.5647° |
| revolutions per day: | 15.27559137 |
| mean anomaly at epoch: | 86.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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