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 54784U 26145.46989308 +.00000000 +00000-0 +54164-3 0 00009
2 54784 53.2124 59.1996 0001442 102.3934 257.7220 15.08797411 07
| Epoch (UTC): | 25 May 2026 11:16:38 |
| Eccentricity: | 0.0001442 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.1996° |
| argument of perigee: | 102.3934° |
| revolutions per day: | 15.08797411 |
| mean anomaly at epoch: | 257.7220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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