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 54764U 26145.15437591 +.00000000 +00000-0 -55783-4 0 00005
2 54764 53.2123 60.7840 0001294 79.5541 280.5597 15.08849375 02
| Epoch (UTC): | 25 May 2026 03:42:18 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 60.7840° |
| argument of perigee: | 79.5541° |
| revolutions per day: | 15.08849375 |
| mean anomaly at epoch: | 280.5597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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