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 26074.65751288 +.00000000 +00000-0 +33293-4 0 00000
2 21667 82.9086 150.7819 0020335 355.3946 156.8366 13.75281612 07
| Epoch (UTC): | 15 March 2026 15:46:49 |
| Eccentricity: | 0.0020335 |
| inclination: | 82.9086° |
| perigee height: | 966 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 150.7819° |
| argument of perigee: | 355.3946° |
| revolutions per day: | 13.75281612 |
| mean anomaly at epoch: | 156.8366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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