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 39476U 26144.95454330 +.00000000 +00000-0 +00000-0 0 00002
2 39476 0.0156 344.8237 0000412 334.0868 329.9068 1.00272076 05
| Epoch (UTC): | 24 May 2026 22:54:32 |
| Eccentricity: | 0.0000412 |
| inclination: | 0.0156° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 344.8237° |
| argument of perigee: | 334.0868° |
| revolutions per day: | 1.00272076 |
| mean anomaly at epoch: | 329.9068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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