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 39133U 26032.42069425 +.00000000 +00000-0 +28692-3 0 00007
2 39133 64.8717 340.7153 0026307 251.2424 108.5850 15.24492974 09
| Epoch (UTC): | 01 February 2026 10:05:47 |
| Eccentricity: | 0.0026307 |
| inclination: | 64.8717° |
| perigee height: | 474 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 340.7153° |
| argument of perigee: | 251.2424° |
| revolutions per day: | 15.24492974 |
| mean anomaly at epoch: | 108.5850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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