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 64164U 26145.42551367 +.00000000 +00000-0 +51430-3 0 00001
2 64164 97.4481 196.7714 0001571 179.5674 180.5555 15.05656087 06
| Epoch (UTC): | 25 May 2026 10:12:44 |
| Eccentricity: | 0.0001571 |
| inclination: | 97.4481° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.7714° |
| argument of perigee: | 179.5674° |
| revolutions per day: | 15.05656087 |
| mean anomaly at epoch: | 180.5555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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