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 51121U 26145.44280839 +.00000000 +00000-0 +55318-4 0 00005
2 51121 53.2154 304.5721 0001511 90.1782 269.9384 15.08839311 09
| Epoch (UTC): | 25 May 2026 10:37:38 |
| Eccentricity: | 0.0001511 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.5721° |
| argument of perigee: | 90.1782° |
| revolutions per day: | 15.08839311 |
| mean anomaly at epoch: | 269.9384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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