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 56327U 26145.45241609 +.00000000 +00000-0 +21706-4 0 00005
2 56327 97.4449 145.3844 0002044 90.0393 270.1068 15.05650422 09
| Epoch (UTC): | 25 May 2026 10:51:28 |
| Eccentricity: | 0.0002044 |
| inclination: | 97.4449° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3844° |
| argument of perigee: | 90.0393° |
| revolutions per day: | 15.05650422 |
| mean anomaly at epoch: | 270.1068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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