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 27632U 26144.32406087 +.00000000 +00000-0 +00000-0 0 00000
2 27632 9.3940 57.1533 0005966 0.3420 191.9185 1.00270898 05
| Epoch (UTC): | 24 May 2026 07:46:38 |
| Eccentricity: | 0.0005966 |
| inclination: | 9.3940° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 57.1533° |
| argument of perigee: | 0.3420° |
| revolutions per day: | 1.00270898 |
| mean anomaly at epoch: | 191.9185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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