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 61959U 26145.38156367 +.00000000 +00000-0 +70670-3 0 00003
2 61959 43.0007 106.3089 0001117 266.4790 93.5934 15.27600491 05
| Epoch (UTC): | 25 May 2026 09:09:27 |
| Eccentricity: | 0.0001117 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.3089° |
| argument of perigee: | 266.4790° |
| revolutions per day: | 15.27600491 |
| mean anomaly at epoch: | 93.5934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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