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 39265U 26031.95065500 +.00000000 +00000-0 +50877-3 0 00000
2 39265 80.9149 231.0070 0327079 158.5773 202.9523 15.15549999 05
| Epoch (UTC): | 31 January 2026 22:48:56 |
| Eccentricity: | 0.0327079 |
| inclination: | 80.9149° |
| perigee height: | 294 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 231.0070° |
| argument of perigee: | 158.5773° |
| revolutions per day: | 15.15549999 |
| mean anomaly at epoch: | 202.9523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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