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 61976U 26145.34571463 +.00000000 +00000-0 +42523-3 0 00002
2 61976 43.0019 106.8970 0001510 269.0353 91.0326 15.27610190 07
| Epoch (UTC): | 25 May 2026 08:17:49 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.8970° |
| argument of perigee: | 269.0353° |
| revolutions per day: | 15.27610190 |
| mean anomaly at epoch: | 91.0326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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