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 60185U 26145.26422544 +.00000000 +00000-0 +91812-6 0 00007
2 60185 53.1579 143.5771 0000941 90.1036 270.0090 15.69700535 02
| Epoch (UTC): | 25 May 2026 06:20:29 |
| Eccentricity: | 0.0000941 |
| inclination: | 53.1579° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 143.5771° |
| argument of perigee: | 90.1036° |
| revolutions per day: | 15.69700535 |
| mean anomaly at epoch: | 270.0090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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