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 60064U 26145.47726703 +.00000000 +00000-0 +12489-4 0 00001
2 60064 53.1595 172.5242 0001115 91.9001 268.2145 15.69703162 05
| Epoch (UTC): | 25 May 2026 11:27:15 |
| Eccentricity: | 0.0001115 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 172.5242° |
| argument of perigee: | 91.9001° |
| revolutions per day: | 15.69703162 |
| mean anomaly at epoch: | 268.2145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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