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 26071.76895676 +.00000000 +00000-0 +11374-4 0 00009
2 20671 82.5518 355.8180 0015243 359.4592 0.6549 13.84734953 00
| Epoch (UTC): | 12 March 2026 18:27:17 |
| Eccentricity: | 0.0015243 |
| inclination: | 82.5518° |
| perigee height: | 936 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 355.8180° |
| argument of perigee: | 359.4592° |
| revolutions per day: | 13.84734953 |
| mean anomaly at epoch: | 0.6549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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