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 59655U 26145.51730899 +.00000000 +00000-0 +83863-4 0 00005
2 59655 42.9997 324.4029 0001415 277.9678 82.1013 15.27578619 09
| Epoch (UTC): | 25 May 2026 12:24:55 |
| Eccentricity: | 0.0001415 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.4029° |
| argument of perigee: | 277.9678° |
| revolutions per day: | 15.27578619 |
| mean anomaly at epoch: | 82.1013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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