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 63782U 26145.52955007 +.00000000 +00000-0 +58992-3 0 00006
2 63782 42.9983 338.5975 0000821 266.7644 93.3114 15.27601593 09
| Epoch (UTC): | 25 May 2026 12:42:33 |
| Eccentricity: | 0.0000821 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.5975° |
| argument of perigee: | 266.7644° |
| revolutions per day: | 15.27601593 |
| mean anomaly at epoch: | 93.3114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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