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 53720U 26145.37328113 +.00000000 +00000-0 +56379-4 0 00000
2 53720 53.2125 269.6292 0001136 28.8183 331.2872 15.08846661 05
| Epoch (UTC): | 25 May 2026 08:57:31 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 269.6292° |
| argument of perigee: | 28.8183° |
| revolutions per day: | 15.08846661 |
| mean anomaly at epoch: | 331.2872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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