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 56343U 26145.24331794 +.00000000 +00000-0 +11165-3 0 00002
2 56343 97.4506 146.2721 0002081 108.7679 251.3774 15.05659694 05
| Epoch (UTC): | 25 May 2026 05:50:22 |
| Eccentricity: | 0.0002081 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.2721° |
| argument of perigee: | 108.7679° |
| revolutions per day: | 15.05659694 |
| mean anomaly at epoch: | 251.3774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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