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 26039.15043288 +.00000000 +00000-0 +23121-4 0 00005
2 20826 82.5257 300.4569 0014121 32.2609 327.9412 13.84451719 08
| Epoch (UTC): | 08 February 2026 03:36:37 |
| Eccentricity: | 0.0014121 |
| inclination: | 82.5257° |
| perigee height: | 938 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 300.4569° |
| argument of perigee: | 32.2609° |
| revolutions per day: | 13.84451719 |
| mean anomaly at epoch: | 327.9412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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