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 64427U 26145.55629641 +.00000000 +00000-0 +29892-3 0 00005
2 64427 70.0006 240.5412 0003310 268.9175 91.1605 14.98341615 05
| Epoch (UTC): | 25 May 2026 13:21:04 |
| Eccentricity: | 0.0003310 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5412° |
| argument of perigee: | 268.9175° |
| revolutions per day: | 14.98341615 |
| mean anomaly at epoch: | 91.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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