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 26071.73918700 +.00000000 +00000-0 +46072-4 0 00009
2 21667 82.9091 152.9548 0020538 3.4989 108.2007 13.75281472 06
| Epoch (UTC): | 12 March 2026 17:44:25 |
| Eccentricity: | 0.0020538 |
| inclination: | 82.9091° |
| perigee height: | 966 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 152.9548° |
| argument of perigee: | 3.4989° |
| revolutions per day: | 13.75281472 |
| mean anomaly at epoch: | 108.2007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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