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 39020U 26145.38387727 +.00000000 +00000-0 +00000-0 0 00000
2 39020 0.0675 14.0787 0004403 41.7820 35.8087 1.00271651 08
| Epoch (UTC): | 25 May 2026 09:12:46 |
| Eccentricity: | 0.0004403 |
| inclination: | 0.0675° |
| perigee height: | 35768 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 14.0787° |
| argument of perigee: | 41.7820° |
| revolutions per day: | 1.00271651 |
| mean anomaly at epoch: | 35.8087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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