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 26064.76578442 +.00000000 +00000-0 +39712-3 0 00007
2 20510 82.5024 335.7324 0005077 322.7770 90.6657 15.15593109 07
| Epoch (UTC): | 05 March 2026 18:22:43 |
| Eccentricity: | 0.0005077 |
| inclination: | 82.5024° |
| perigee height: | 516 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 335.7324° |
| argument of perigee: | 322.7770° |
| revolutions per day: | 15.15593109 |
| mean anomaly at epoch: | 90.6657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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