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 60183U 26145.27402133 +.00000000 +00000-0 +10036-4 0 00005
2 60183 53.1592 143.6352 0001099 119.9909 240.1218 15.69718729 09
| Epoch (UTC): | 25 May 2026 06:34:35 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 143.6352° |
| argument of perigee: | 119.9909° |
| revolutions per day: | 15.69718729 |
| mean anomaly at epoch: | 240.1218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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