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 67779U 26145.58335647 +.00000000 +00000-0 -11245+0 0 00001
2 67779 51.8934 210.7474 0010491 347.9830 166.7134 15.06860477 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0010491 |
| inclination: | 51.8934° |
| perigee height: | 539 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 210.7474° |
| argument of perigee: | 347.9830° |
| revolutions per day: | 15.06860477 |
| mean anomaly at epoch: | 166.7134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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