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 26906U 26020.81949985 +.00000000 +00000-0 +16826-3 0 00005
2 26906 63.4210 178.2616 0615684 341.4346 16.5072 13.45127782 08
| Epoch (UTC): | 20 January 2026 19:40:04 |
| Eccentricity: | 0.0615684 |
| inclination: | 63.4210° |
| perigee height: | 630 km |
| apogee height: | 1550 km |
| right ascension of ascending node: | 178.2616° |
| argument of perigee: | 341.4346° |
| revolutions per day: | 13.45127782 |
| mean anomaly at epoch: | 16.5072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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