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 53984U 26145.21878312 +.00000000 +00000-0 +75583-4 0 00004
2 53984 53.2118 230.7218 0001126 89.2675 270.8446 15.08830777 08
| Epoch (UTC): | 25 May 2026 05:15:02 |
| Eccentricity: | 0.0001126 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 230.7218° |
| argument of perigee: | 89.2675° |
| revolutions per day: | 15.08830777 |
| mean anomaly at epoch: | 270.8446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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