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 57703U 26145.06752995 +.00000000 +00000-0 +19999-3 0 00006
2 57703 43.0032 46.5632 0001293 261.0871 98.9834 15.27559506 08
| Epoch (UTC): | 25 May 2026 01:37:14 |
| Eccentricity: | 0.0001293 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.5632° |
| argument of perigee: | 261.0871° |
| revolutions per day: | 15.27559506 |
| mean anomaly at epoch: | 98.9834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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