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 54774U 26145.45837385 +.00000000 +00000-0 +28184-3 0 00007
2 54774 53.2139 44.1697 0001379 97.9383 262.1766 15.08818699 07
| Epoch (UTC): | 25 May 2026 11:00:03 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.1697° |
| argument of perigee: | 97.9383° |
| revolutions per day: | 15.08818699 |
| mean anomaly at epoch: | 262.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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