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 53532U 26145.24266839 +.00000000 +00000-0 +78097-4 0 00004
2 53532 53.2149 90.4571 0001430 68.5824 291.5321 15.08843862 09
| Epoch (UTC): | 25 May 2026 05:49:26 |
| Eccentricity: | 0.0001430 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.4571° |
| argument of perigee: | 68.5824° |
| revolutions per day: | 15.08843862 |
| mean anomaly at epoch: | 291.5321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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