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 62669U 26145.63685081 +.00000000 +00000-0 +15856-3 0 00005
2 62669 97.4032 225.3456 0006694 70.8880 289.3080 15.22150120 08
| Epoch (UTC): | 25 May 2026 15:17:03 |
| Eccentricity: | 0.0006694 |
| inclination: | 97.4032° |
| perigee height: | 495 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 225.3456° |
| argument of perigee: | 70.8880° |
| revolutions per day: | 15.22150120 |
| mean anomaly at epoch: | 289.3080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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