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 53778U 26145.42065352 +.00000000 +00000-0 -20811-4 0 00005
2 53778 53.2136 294.3879 0001567 88.8142 271.3030 15.08844195 05
| Epoch (UTC): | 25 May 2026 10:05:44 |
| Eccentricity: | 0.0001567 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.3879° |
| argument of perigee: | 88.8142° |
| revolutions per day: | 15.08844195 |
| mean anomaly at epoch: | 271.3030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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