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 21667U 26075.67635573 +.00000000 +00000-0 +39547-4 0 00009
2 21667 82.9083 150.0233 0020270 352.4980 161.1968 13.75281702 08
| Epoch (UTC): | 16 March 2026 16:13:57 |
| Eccentricity: | 0.0020270 |
| inclination: | 82.9083° |
| perigee height: | 966 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 150.0233° |
| argument of perigee: | 352.4980° |
| revolutions per day: | 13.75281702 |
| mean anomaly at epoch: | 161.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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