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 55076U 26145.13099435 +.00000000 +00000-0 +27753-3 0 00005
2 55076 97.3211 208.2323 0008966 180.7391 179.3842 15.37998877 04
| Epoch (UTC): | 25 May 2026 03:08:37 |
| Eccentricity: | 0.0008966 |
| inclination: | 97.3211° |
| perigee height: | 446 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 208.2323° |
| argument of perigee: | 180.7391° |
| revolutions per day: | 15.37998877 |
| mean anomaly at epoch: | 179.3842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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