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 62655U 26145.49086711 +.00000000 +00000-0 +60387-3 0 00008
2 62655 97.4032 231.6238 0001074 64.3559 295.7798 15.40141568 02
| Epoch (UTC): | 25 May 2026 11:46:50 |
| Eccentricity: | 0.0001074 |
| inclination: | 97.4032° |
| perigee height: | 445 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 231.6238° |
| argument of perigee: | 64.3559° |
| revolutions per day: | 15.40141568 |
| mean anomaly at epoch: | 295.7798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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