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 39452U 26031.88236772 +.00000000 +00000-0 +20628-3 0 00002
2 39452 87.3352 106.7798 0002830 93.8068 266.3515 15.47862564 04
| Epoch (UTC): | 31 January 2026 21:10:36 |
| Eccentricity: | 0.0002830 |
| inclination: | 87.3352° |
| perigee height: | 421 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 106.7798° |
| argument of perigee: | 93.8068° |
| revolutions per day: | 15.47862564 |
| mean anomaly at epoch: | 266.3515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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