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 56308U 26145.38208227 +.00000000 +00000-0 +12426-3 0 00003
2 56308 9.8886 67.6731 0020985 327.9410 31.9526 14.94905169 07
| Epoch (UTC): | 25 May 2026 09:10:11 |
| Eccentricity: | 0.0020985 |
| inclination: | 9.8886° |
| perigee height: | 568 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 67.6731° |
| argument of perigee: | 327.9410° |
| revolutions per day: | 14.94905169 |
| mean anomaly at epoch: | 31.9526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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