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 26159.48851181 +.00000000 +00000-0 +22385-4 0 00002
2 20671 82.5471 286.0685 0016543 106.8096 253.4881 13.84738738 02
| Epoch (UTC): | 08 June 2026 11:43:27 |
| Eccentricity: | 0.0016543 |
| inclination: | 82.5471° |
| perigee height: | 935 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 286.0685° |
| argument of perigee: | 106.8096° |
| revolutions per day: | 13.84738738 |
| mean anomaly at epoch: | 253.4881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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