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 54178U 26145.60602877 +.00000000 +00000-0 +10780-4 0 00002
2 54178 53.2145 18.5063 0001391 91.0608 269.0543 15.08838392 04
| Epoch (UTC): | 25 May 2026 14:32:40 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 18.5063° |
| argument of perigee: | 91.0608° |
| revolutions per day: | 15.08838392 |
| mean anomaly at epoch: | 269.0543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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