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 51862U 26144.96712564 +.00000000 +00000-0 -18395-3 0 00002
2 51862 53.2126 26.6962 0001371 97.3760 262.7388 15.08854089 02
| Epoch (UTC): | 24 May 2026 23:12:39 |
| Eccentricity: | 0.0001371 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.6962° |
| argument of perigee: | 97.3760° |
| revolutions per day: | 15.08854089 |
| mean anomaly at epoch: | 262.7388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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