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 62609U 26145.49432866 +.00000000 +00000-0 +29396-3 0 00008
2 62609 97.3927 224.1438 0009055 62.4509 297.7646 15.21369408 01
| Epoch (UTC): | 25 May 2026 11:51:49 |
| Eccentricity: | 0.0009055 |
| inclination: | 97.3927° |
| perigee height: | 495 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 224.1438° |
| argument of perigee: | 62.4509° |
| revolutions per day: | 15.21369408 |
| mean anomaly at epoch: | 297.7646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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