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 56003U 26144.97735638 +.00000000 +00000-0 +21655-4 0 00005
2 56003 43.0040 349.0223 0001794 246.5987 113.4677 15.27576098 01
| Epoch (UTC): | 24 May 2026 23:27:23 |
| Eccentricity: | 0.0001794 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.0223° |
| argument of perigee: | 246.5987° |
| revolutions per day: | 15.27576098 |
| mean anomaly at epoch: | 113.4677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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