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 56743U 26145.63677491 +.00000000 +00000-0 +25289-3 0 00008
2 56743 97.5267 342.4224 0007355 99.1764 261.0307 15.27463689 00
| Epoch (UTC): | 25 May 2026 15:16:57 |
| Eccentricity: | 0.0007355 |
| inclination: | 97.5267° |
| perigee height: | 478 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 342.4224° |
| argument of perigee: | 99.1764° |
| revolutions per day: | 15.27463689 |
| mean anomaly at epoch: | 261.0307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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