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 20682U 26017.97954365 +.00000000 +00000-0 +50098-3 0 00000
2 20682 63.2931 254.2051 0882120 80.0607 289.8723 13.63737316 04
| Epoch (UTC): | 17 January 2026 23:30:32 |
| Eccentricity: | 0.0882120 |
| inclination: | 63.2931° |
| perigee height: | 369 km |
| apogee height: | 1675 km |
| right ascension of ascending node: | 254.2051° |
| argument of perigee: | 80.0607° |
| revolutions per day: | 13.63737316 |
| mean anomaly at epoch: | 289.8723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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