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 26069.20783314 +.00000000 +00000-0 +29985-3 0 00008
2 20510 82.5016 331.3470 0004958 302.5624 212.3915 15.15652462 01
| Epoch (UTC): | 10 March 2026 04:59:16 |
| Eccentricity: | 0.0004958 |
| inclination: | 82.5016° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 331.3470° |
| argument of perigee: | 302.5624° |
| revolutions per day: | 15.15652462 |
| mean anomaly at epoch: | 212.3915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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