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 51778U 26145.57063862 +.00000000 +00000-0 +95680-4 0 00008
2 51778 53.2109 343.8635 0001050 83.3143 276.7969 15.08848854 07
| Epoch (UTC): | 25 May 2026 13:41:43 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.2109° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 343.8635° |
| argument of perigee: | 83.3143° |
| revolutions per day: | 15.08848854 |
| mean anomaly at epoch: | 276.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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