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 60724U 26145.28753132 +.00000000 +00000-0 +26864-4 0 00001
2 60724 53.1563 98.8028 0001058 78.5545 281.5591 15.69712802 09
| Epoch (UTC): | 25 May 2026 06:54:02 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1563° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.8028° |
| argument of perigee: | 78.5545° |
| revolutions per day: | 15.69712802 |
| mean anomaly at epoch: | 281.5591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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