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 26064.76006661 +.00000000 +00000-0 +27246-4 0 00004
2 20671 82.5513 1.3876 0015690 18.9384 341.2357 13.84734566 03
| Epoch (UTC): | 05 March 2026 18:14:29 |
| Eccentricity: | 0.0015690 |
| inclination: | 82.5513° |
| perigee height: | 936 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 1.3876° |
| argument of perigee: | 18.9384° |
| revolutions per day: | 13.84734566 |
| mean anomaly at epoch: | 341.2357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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