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 13066U 26064.26101500 +.00000000 +00000-0 +64616-4 0 00009
2 13066 82.9015 358.1852 0043017 333.0300 180.8588 13.77378514 06
| Epoch (UTC): | 05 March 2026 06:15:51 |
| Eccentricity: | 0.0043017 |
| inclination: | 82.9015° |
| perigee height: | 942 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 358.1852° |
| argument of perigee: | 333.0300° |
| revolutions per day: | 13.77378514 |
| mean anomaly at epoch: | 180.8588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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