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 60732U 26145.24337708 +.00000000 +00000-0 +13719-4 0 00008
2 60732 53.1589 98.4934 0001184 120.9380 239.1754 15.69711234 05
| Epoch (UTC): | 25 May 2026 05:50:27 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 98.4934° |
| argument of perigee: | 120.9380° |
| revolutions per day: | 15.69711234 |
| mean anomaly at epoch: | 239.1754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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