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 53261U 26145.44138676 +.00000000 +00000-0 +47296-4 0 00009
2 53261 53.2125 209.5695 0000818 86.5900 273.5186 15.08838751 06
| Epoch (UTC): | 25 May 2026 10:35:35 |
| Eccentricity: | 0.0000818 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.5695° |
| argument of perigee: | 86.5900° |
| revolutions per day: | 15.08838751 |
| mean anomaly at epoch: | 273.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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