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 60911U 26145.15405417 +.00000000 +00000-0 +76243-5 0 00002
2 60911 53.1585 114.3462 0000899 97.1216 262.9904 15.69706950 09
| Epoch (UTC): | 25 May 2026 03:41:50 |
| Eccentricity: | 0.0000899 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 114.3462° |
| argument of perigee: | 97.1216° |
| revolutions per day: | 15.69706950 |
| mean anomaly at epoch: | 262.9904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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