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 62607U 26145.48575162 +.00000000 +00000-0 +19547-2 0 00008
2 62607 42.9941 196.0167 0015882 58.4577 301.7829 15.43958826 03
| Epoch (UTC): | 25 May 2026 11:39:28 |
| Eccentricity: | 0.0015882 |
| inclination: | 42.9941° |
| perigee height: | 424 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 196.0167° |
| argument of perigee: | 58.4577° |
| revolutions per day: | 15.43958826 |
| mean anomaly at epoch: | 301.7829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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