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 58867U 26145.44736064 +.00000000 +00000-0 +36716-3 0 00005
2 58867 42.9994 175.2343 0001036 247.4156 112.6586 15.27532164 02
| Epoch (UTC): | 25 May 2026 10:44:11 |
| Eccentricity: | 0.0001036 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2343° |
| argument of perigee: | 247.4156° |
| revolutions per day: | 15.27532164 |
| mean anomaly at epoch: | 112.6586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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