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 64432U 26145.54377579 +.00000000 +00000-0 +89969-4 0 00002
2 64432 70.0005 240.5019 0003335 268.4210 91.6567 14.98342133 03
| Epoch (UTC): | 25 May 2026 13:03:02 |
| Eccentricity: | 0.0003335 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5019° |
| argument of perigee: | 268.4210° |
| revolutions per day: | 14.98342133 |
| mean anomaly at epoch: | 91.6567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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