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 26066.28695331 +.00000000 +00000-0 +82738-4 0 00008
2 13066 82.9016 356.6695 0042909 327.2471 146.7157 13.77378897 05
| Epoch (UTC): | 07 March 2026 06:53:12 |
| Eccentricity: | 0.0042909 |
| inclination: | 82.9016° |
| perigee height: | 942 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 356.6695° |
| argument of perigee: | 327.2471° |
| revolutions per day: | 13.77378897 |
| mean anomaly at epoch: | 146.7157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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