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 39072U 26145.43673183 +.00000000 +00000-0 +78271-4 0 00006
2 39072 52.0056 312.5882 0000616 104.7253 255.3682 12.62251198 03
| Epoch (UTC): | 25 May 2026 10:28:53 |
| Eccentricity: | 0.0000616 |
| inclination: | 52.0056° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 312.5882° |
| argument of perigee: | 104.7253° |
| revolutions per day: | 12.62251198 |
| mean anomaly at epoch: | 255.3682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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