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 20510U 26072.68397507 +.00000000 +00000-0 +26322-3 0 00001
2 20510 82.5013 327.9142 0004623 288.7093 101.4616 15.15686876 01
| Epoch (UTC): | 13 March 2026 16:24:55 |
| Eccentricity: | 0.0004623 |
| inclination: | 82.5013° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 327.9142° |
| argument of perigee: | 288.7093° |
| revolutions per day: | 15.15686876 |
| mean anomaly at epoch: | 101.4616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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