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 56472U 26145.36705506 +.00000000 +00000-0 +28015-3 0 00006
2 56472 69.9988 291.1718 0002949 272.2175 87.8646 14.98322700 09
| Epoch (UTC): | 25 May 2026 08:48:33 |
| Eccentricity: | 0.0002949 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.1718° |
| argument of perigee: | 272.2175° |
| revolutions per day: | 14.98322700 |
| mean anomaly at epoch: | 87.8646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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