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 26072.94512215 +.00000000 +00000-0 +11590-3 0 00005
2 06966 74.0540 58.4267 0021872 305.9558 53.9571 14.44827230 01
| Epoch (UTC): | 13 March 2026 22:40:58 |
| Eccentricity: | 0.0021872 |
| inclination: | 74.0540° |
| perigee height: | 727 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 58.4267° |
| argument of perigee: | 305.9558° |
| revolutions per day: | 14.44827230 |
| mean anomaly at epoch: | 53.9571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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