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 20671U 26065.77165926 +.00000000 +00000-0 +34039-4 0 00004
2 20671 82.5514 0.5836 0015630 16.2065 343.9592 13.84734642 07
| Epoch (UTC): | 06 March 2026 18:31:11 |
| Eccentricity: | 0.0015630 |
| inclination: | 82.5514° |
| perigee height: | 936 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 0.5836° |
| argument of perigee: | 16.2065° |
| revolutions per day: | 13.84734642 |
| mean anomaly at epoch: | 343.9592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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