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 60547U 26145.51817918 +.00000000 +00000-0 +81258-3 0 00000
2 60547 97.6971 232.3759 0001907 93.4703 266.6748 15.17234763 05
| Epoch (UTC): | 25 May 2026 12:26:10 |
| Eccentricity: | 0.0001907 |
| inclination: | 97.6971° |
| perigee height: | 513 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 232.3759° |
| argument of perigee: | 93.4703° |
| revolutions per day: | 15.17234763 |
| mean anomaly at epoch: | 266.6748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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