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 39679U 26049.40593809 +.00000000 +00000-0 +29548-3 0 00007
2 39679 51.6060 71.3036 0098825 32.6899 328.0149 15.38504324 05
| Epoch (UTC): | 18 February 2026 09:44:33 |
| Eccentricity: | 0.0098825 |
| inclination: | 51.6060° |
| perigee height: | 383 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 71.3036° |
| argument of perigee: | 32.6899° |
| revolutions per day: | 15.38504324 |
| mean anomaly at epoch: | 328.0149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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