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 64169U 26145.57504313 +.00000000 +00000-0 +17731-3 0 00007
2 64169 97.4495 196.8775 0001775 127.0563 233.0827 15.05654338 08
| Epoch (UTC): | 25 May 2026 13:48:03 |
| Eccentricity: | 0.0001775 |
| inclination: | 97.4495° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.8775° |
| argument of perigee: | 127.0563° |
| revolutions per day: | 15.05654338 |
| mean anomaly at epoch: | 233.0827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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