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 56508U 26145.44926831 +.00000000 +00000-0 +60134-4 0 00000
2 56508 43.0030 138.5961 0001479 264.2024 95.8659 15.27581557 08
| Epoch (UTC): | 25 May 2026 10:46:56 |
| Eccentricity: | 0.0001479 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.5961° |
| argument of perigee: | 264.2024° |
| revolutions per day: | 15.27581557 |
| mean anomaly at epoch: | 95.8659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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