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 56688U 26145.42838299 +.00000000 +00000-0 -99879-5 0 00007
2 56688 43.0015 204.6764 0001152 256.0622 104.0101 15.27579675 00
| Epoch (UTC): | 25 May 2026 10:16:52 |
| Eccentricity: | 0.0001152 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.6764° |
| argument of perigee: | 256.0622° |
| revolutions per day: | 15.27579675 |
| mean anomaly at epoch: | 104.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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