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 54204U 26145.32726222 +.00000000 +00000-0 +77654-4 0 00005
2 54204 53.2141 9.6473 0001232 82.4323 277.6809 15.08829595 03
| Epoch (UTC): | 25 May 2026 07:51:15 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.6473° |
| argument of perigee: | 82.4323° |
| revolutions per day: | 15.08829595 |
| mean anomaly at epoch: | 277.6809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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