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 55988U 26145.27053587 +.00000000 +00000-0 +25637-4 0 00000
2 55988 43.0030 351.2093 0001199 270.3625 89.7089 15.27578067 04
| Epoch (UTC): | 25 May 2026 06:29:34 |
| Eccentricity: | 0.0001199 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 351.2093° |
| argument of perigee: | 270.3625° |
| revolutions per day: | 15.27578067 |
| mean anomaly at epoch: | 89.7089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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