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 56326U 26145.47456227 +.00000000 +00000-0 +91983-4 0 00004
2 56326 97.4483 145.3550 0002388 88.5902 271.5599 15.05645307 09
| Epoch (UTC): | 25 May 2026 11:23:22 |
| Eccentricity: | 0.0002388 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3550° |
| argument of perigee: | 88.5902° |
| revolutions per day: | 15.05645307 |
| mean anomaly at epoch: | 271.5599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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