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 53703U 26145.56923698 +.00000000 +00000-0 +72583-4 0 00006
2 53703 53.2143 258.7378 0001278 84.8859 275.2279 15.08838866 05
| Epoch (UTC): | 25 May 2026 13:39:42 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 258.7378° |
| argument of perigee: | 84.8859° |
| revolutions per day: | 15.08838866 |
| mean anomaly at epoch: | 275.2279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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