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 62311U 26145.37751119 +.00000000 +00000-0 +32914-3 0 00000
2 62311 53.1596 185.0378 0001223 88.1142 271.9999 15.30203532 08
| Epoch (UTC): | 25 May 2026 09:03:36 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 185.0378° |
| argument of perigee: | 88.1142° |
| revolutions per day: | 15.30203532 |
| mean anomaly at epoch: | 271.9999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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