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 64423U 26145.36854296 +.00000000 +00000-0 +23534-3 0 00003
2 64423 70.0004 241.0959 0003313 269.6730 90.4050 14.98336454 00
| Epoch (UTC): | 25 May 2026 08:50:42 |
| Eccentricity: | 0.0003313 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 241.0959° |
| argument of perigee: | 269.6730° |
| revolutions per day: | 14.98336454 |
| mean anomaly at epoch: | 90.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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