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 56881U 26144.91653801 +.00000000 +00000-0 +23822-4 0 00002
2 56881 43.0028 15.1038 0001347 248.2009 111.8700 15.27578069 03
| Epoch (UTC): | 24 May 2026 21:59:48 |
| Eccentricity: | 0.0001347 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 15.1038° |
| argument of perigee: | 248.2009° |
| revolutions per day: | 15.27578069 |
| mean anomaly at epoch: | 111.8700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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