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 62127U 26145.15129374 +.00000000 +00000-0 +11173-2 0 00006
2 62127 43.0014 53.7632 0001752 267.0989 92.9662 15.27602945 09
| Epoch (UTC): | 25 May 2026 03:37:51 |
| Eccentricity: | 0.0001752 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.7632° |
| argument of perigee: | 267.0989° |
| revolutions per day: | 15.27602945 |
| mean anomaly at epoch: | 92.9662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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