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 52577U 26145.30339355 +.00000000 +00000-0 -11749-3 0 00004
2 52577 53.2117 150.1890 0001492 77.9088 282.2071 15.08848421 09
| Epoch (UTC): | 25 May 2026 07:16:53 |
| Eccentricity: | 0.0001492 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.1890° |
| argument of perigee: | 77.9088° |
| revolutions per day: | 15.08848421 |
| mean anomaly at epoch: | 282.2071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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