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 64444U 26145.11225968 +.00000000 +00000-0 +59097-3 0 00000
2 64444 53.1603 92.8602 0001050 86.8761 273.2361 15.34401389 03
| Epoch (UTC): | 25 May 2026 02:41:39 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.8602° |
| argument of perigee: | 86.8761° |
| revolutions per day: | 15.34401389 |
| mean anomaly at epoch: | 273.2361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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