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 51632U 26145.13562295 +.00000000 +00000-0 -80179-3 0 00000
2 51632 87.8854 40.8677 0001726 72.2251 287.9064 13.10376418 06
| Epoch (UTC): | 25 May 2026 03:15:17 |
| Eccentricity: | 0.0001726 |
| inclination: | 87.8854° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8677° |
| argument of perigee: | 72.2251° |
| revolutions per day: | 13.10376418 |
| mean anomaly at epoch: | 287.9064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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