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 28474U 26145.36143050 +.00000000 +00000-0 +00000-0 0 00008
2 28474 55.1498 325.8150 0169831 315.8284 41.4155 2.00554891 06
| Epoch (UTC): | 25 May 2026 08:40:27 |
| Eccentricity: | 0.0169831 |
| inclination: | 55.1498° |
| perigee height: | 19732 km |
| apogee height: | 20634 km |
| right ascension of ascending node: | 325.8150° |
| argument of perigee: | 315.8284° |
| revolutions per day: | 2.00554891 |
| mean anomaly at epoch: | 41.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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