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 60563U 26145.18233361 +.00000000 +00000-0 +39609-3 0 00008
2 60563 97.3742 230.3128 0004076 35.3207 324.8310 15.43244270 03
| Epoch (UTC): | 25 May 2026 04:22:33 |
| Eccentricity: | 0.0004076 |
| inclination: | 97.3742° |
| perigee height: | 434 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 230.3128° |
| argument of perigee: | 35.3207° |
| revolutions per day: | 15.43244270 |
| mean anomaly at epoch: | 324.8310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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