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 60585U 26145.47105314 +.00000000 +00000-0 +45799-4 0 00008
2 60585 53.1617 310.6194 0001213 77.4312 282.6825 15.30192048 00
| Epoch (UTC): | 25 May 2026 11:18:18 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6194° |
| argument of perigee: | 77.4312° |
| revolutions per day: | 15.30192048 |
| mean anomaly at epoch: | 282.6825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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