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 06966U 26065.46713734 +.00000000 +00000-0 +12650-3 0 00001
2 06966 74.0531 72.3380 0021658 321.0912 38.8685 14.44820581 07
| Epoch (UTC): | 06 March 2026 11:12:40 |
| Eccentricity: | 0.0021658 |
| inclination: | 74.0531° |
| perigee height: | 727 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 72.3380° |
| argument of perigee: | 321.0912° |
| revolutions per day: | 14.44820581 |
| mean anomaly at epoch: | 38.8685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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