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 53807U 26129.51521126 +.00000000 +00000-0 +12700-3 0 00002
2 53807 53.2282 215.4542 0007278 61.8497 298.3243 15.37812167 01
| Epoch (UTC): | 09 May 2026 12:21:54 |
| Eccentricity: | 0.0007278 |
| inclination: | 53.2282° |
| perigee height: | 448 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 215.4542° |
| argument of perigee: | 61.8497° |
| revolutions per day: | 15.37812167 |
| mean anomaly at epoch: | 298.3243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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