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 64418U 26145.40210182 +.00000000 +00000-0 +18872-3 0 00001
2 64418 70.0006 241.2100 0003233 270.3013 89.7775 14.98334042 06
| Epoch (UTC): | 25 May 2026 09:39:01 |
| Eccentricity: | 0.0003233 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 241.2100° |
| argument of perigee: | 270.3013° |
| revolutions per day: | 14.98334042 |
| mean anomaly at epoch: | 89.7775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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