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 47262U 26145.28314213 +.00000000 +00000-0 -15547-4 0 00003
2 47262 87.8962 355.2133 0001724 94.4901 265.6424 13.12441696 02
| Epoch (UTC): | 25 May 2026 06:47:43 |
| Eccentricity: | 0.0001724 |
| inclination: | 87.8962° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2133° |
| argument of perigee: | 94.4901° |
| revolutions per day: | 13.12441696 |
| mean anomaly at epoch: | 265.6424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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