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 64160U 26145.42274461 +.00000000 +00000-0 +41045-3 0 00005
2 64160 97.4482 196.7768 0001144 157.6374 202.4903 15.05656495 06
| Epoch (UTC): | 25 May 2026 10:08:45 |
| Eccentricity: | 0.0001144 |
| inclination: | 97.4482° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 196.7768° |
| argument of perigee: | 157.6374° |
| revolutions per day: | 15.05656495 |
| mean anomaly at epoch: | 202.4903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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