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 62057U 26145.45768501 +.00000000 +00000-0 +19265-2 0 00002
2 62057 53.1571 52.6117 0003245 75.9102 284.2276 15.69780389 01
| Epoch (UTC): | 25 May 2026 10:59:03 |
| Eccentricity: | 0.0003245 |
| inclination: | 53.1571° |
| perigee height: | 357 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 52.6117° |
| argument of perigee: | 75.9102° |
| revolutions per day: | 15.69780389 |
| mean anomaly at epoch: | 284.2276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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