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 64417U 26145.55212461 +.00000000 +00000-0 +41190-3 0 00007
2 64417 70.0005 240.5327 0003277 270.4843 89.5941 14.98340424 01
| Epoch (UTC): | 25 May 2026 13:15:03 |
| Eccentricity: | 0.0003277 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5327° |
| argument of perigee: | 270.4843° |
| revolutions per day: | 14.98340424 |
| mean anomaly at epoch: | 89.5941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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