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 26075.65353492 +.00000000 +00000-0 +20276-3 0 00008
2 20510 82.5006 324.9820 0004466 274.1458 109.2095 15.15713162 08
| Epoch (UTC): | 16 March 2026 15:41:05 |
| Eccentricity: | 0.0004466 |
| inclination: | 82.5006° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 324.9820° |
| argument of perigee: | 274.1458° |
| revolutions per day: | 15.15713162 |
| mean anomaly at epoch: | 109.2095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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