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 39612U 26145.59560182 +.00000000 +00000-0 +00000-0 0 00008
2 39612 0.2010 85.7819 0003016 29.4530 42.2938 1.00297667 03
| Epoch (UTC): | 25 May 2026 14:17:39 |
| Eccentricity: | 0.0003016 |
| inclination: | 0.2010° |
| perigee height: | 35767 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 85.7819° |
| argument of perigee: | 29.4530° |
| revolutions per day: | 1.00297667 |
| mean anomaly at epoch: | 42.2938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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