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 54767U 26145.48830384 +.00000000 +00000-0 +50222-5 0 00004
2 54767 53.2128 59.3111 0001356 90.6134 269.5014 15.08838325 00
| Epoch (UTC): | 25 May 2026 11:43:09 |
| Eccentricity: | 0.0001356 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.3111° |
| argument of perigee: | 90.6134° |
| revolutions per day: | 15.08838325 |
| mean anomaly at epoch: | 269.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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