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 63778U 26144.94492918 +.00000000 +00000-0 +85898-3 0 00008
2 63778 43.0041 341.9531 0002226 279.1853 80.8746 15.27593495 01
| Epoch (UTC): | 24 May 2026 22:40:41 |
| Eccentricity: | 0.0002226 |
| inclination: | 43.0041° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 341.9531° |
| argument of perigee: | 279.1853° |
| revolutions per day: | 15.27593495 |
| mean anomaly at epoch: | 80.8746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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