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 64173U 26145.30126946 +.00000000 +00000-0 +43162-3 0 00002
2 64173 53.1568 94.6478 0000817 111.6328 248.4760 15.31717323 01
| Epoch (UTC): | 25 May 2026 07:13:49 |
| Eccentricity: | 0.0000817 |
| inclination: | 53.1568° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 94.6478° |
| argument of perigee: | 111.6328° |
| revolutions per day: | 15.31717323 |
| mean anomaly at epoch: | 248.4760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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