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 56506U 26145.35449424 +.00000000 +00000-0 +16103-3 0 00002
2 56506 43.0034 128.2954 0001623 274.6978 85.3689 15.27556197 01
| Epoch (UTC): | 25 May 2026 08:30:28 |
| Eccentricity: | 0.0001623 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.2954° |
| argument of perigee: | 274.6978° |
| revolutions per day: | 15.27556197 |
| mean anomaly at epoch: | 85.3689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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