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 20826U 26088.00586438 +.00000000 +00000-0 +51159-4 0 00004
2 20826 82.5207 261.5030 0012235 248.8415 111.1438 13.84454414 03
| Epoch (UTC): | 29 March 2026 00:08:26 |
| Eccentricity: | 0.0012235 |
| inclination: | 82.5207° |
| perigee height: | 939 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 261.5030° |
| argument of perigee: | 248.8415° |
| revolutions per day: | 13.84454414 |
| mean anomaly at epoch: | 111.1438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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