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 53588U 26145.34482132 +.00000000 +00000-0 +14195-5 0 00002
2 53588 53.2148 260.2498 0001198 88.2915 271.8214 15.08832841 02
| Epoch (UTC): | 25 May 2026 08:16:32 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 260.2498° |
| argument of perigee: | 88.2915° |
| revolutions per day: | 15.08832841 |
| mean anomaly at epoch: | 271.8214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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