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 26069.31223259 +.00000000 +00000-0 +32927-4 0 00006
2 20671 82.5518 357.7702 0015402 6.3555 353.7798 13.84734921 08
| Epoch (UTC): | 10 March 2026 07:29:36 |
| Eccentricity: | 0.0015402 |
| inclination: | 82.5518° |
| perigee height: | 936 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 357.7702° |
| argument of perigee: | 6.3555° |
| revolutions per day: | 13.84734921 |
| mean anomaly at epoch: | 353.7798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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