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 39439U 26044.94037918 +.00000000 +00000-0 +23766-2 0 00004
2 39439 97.7393 40.6929 0014519 144.7374 215.4859 15.86869189 03
| Epoch (UTC): | 13 February 2026 22:34:08 |
| Eccentricity: | 0.0014519 |
| inclination: | 97.7393° |
| perigee height: | 301 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 40.6929° |
| argument of perigee: | 144.7374° |
| revolutions per day: | 15.86869189 |
| mean anomaly at epoch: | 215.4859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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