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 54787U 26145.46619507 +.00000000 +00000-0 +58965-4 0 00007
2 54787 53.2131 59.1760 0001251 87.2757 272.8378 15.08837040 04
| Epoch (UTC): | 25 May 2026 11:11:19 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.1760° |
| argument of perigee: | 87.2757° |
| revolutions per day: | 15.08837040 |
| mean anomaly at epoch: | 272.8378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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