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 62616U 26145.46911787 +.00000000 +00000-0 +28039-3 0 00000
2 62616 97.3905 225.7046 0007116 63.0250 297.1714 15.26131643 06
| Epoch (UTC): | 25 May 2026 11:15:31 |
| Eccentricity: | 0.0007116 |
| inclination: | 97.3905° |
| perigee height: | 483 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 225.7046° |
| argument of perigee: | 63.0250° |
| revolutions per day: | 15.26131643 |
| mean anomaly at epoch: | 297.1714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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