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 56842U 26145.10992700 +.00000000 +00000-0 +58532-4 0 00001
2 56842 43.0015 35.5520 0001305 261.4671 98.6033 15.27574667 05
| Epoch (UTC): | 25 May 2026 02:38:17 |
| Eccentricity: | 0.0001305 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.5520° |
| argument of perigee: | 261.4671° |
| revolutions per day: | 15.27574667 |
| mean anomaly at epoch: | 98.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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