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 05732U 26039.13380308 +.00000000 +00000-0 +53766-4 0 00007
2 05732 81.2539 312.0310 0051081 162.0459 198.2529 14.06412550 03
| Epoch (UTC): | 08 February 2026 03:12:40 |
| Eccentricity: | 0.0051081 |
| inclination: | 81.2539° |
| perigee height: | 835 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 312.0310° |
| argument of perigee: | 162.0459° |
| revolutions per day: | 14.06412550 |
| mean anomaly at epoch: | 198.2529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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