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 62475U 26144.79127698 +.00000000 +00000-0 +86869-3 0 00003
2 62475 43.0016 309.8912 0001735 274.7461 85.3193 15.27601531 09
| Epoch (UTC): | 24 May 2026 18:59:26 |
| Eccentricity: | 0.0001735 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8912° |
| argument of perigee: | 274.7461° |
| revolutions per day: | 15.27601531 |
| mean anomaly at epoch: | 85.3193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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