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 67772U 26145.44615110 +.00000000 +00000-0 +45916-3 0 00000
2 67772 51.8836 213.5798 0002770 20.5924 339.5166 15.18810645 07
| Epoch (UTC): | 25 May 2026 10:42:27 |
| Eccentricity: | 0.0002770 |
| inclination: | 51.8836° |
| perigee height: | 508 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 213.5798° |
| argument of perigee: | 20.5924° |
| revolutions per day: | 15.18810645 |
| mean anomaly at epoch: | 339.5166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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