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 63857U 26145.32248179 +.00000000 +00000-0 +58689-3 0 00005
2 63857 43.0008 4.9564 0001297 274.0032 86.0671 15.27590856 07
| Epoch (UTC): | 25 May 2026 07:44:22 |
| Eccentricity: | 0.0001297 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9564° |
| argument of perigee: | 274.0032° |
| revolutions per day: | 15.27590856 |
| mean anomaly at epoch: | 86.0671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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