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 56029U 26145.48554330 +.00000000 +00000-0 -58657-4 0 00001
2 56029 43.0036 331.2441 0001284 262.5619 97.5087 15.27576967 05
| Epoch (UTC): | 25 May 2026 11:39:10 |
| Eccentricity: | 0.0001284 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.2441° |
| argument of perigee: | 262.5619° |
| revolutions per day: | 15.27576967 |
| mean anomaly at epoch: | 97.5087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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