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 64442U 26145.54094704 +.00000000 +00000-0 +78201-3 0 00005
2 64442 53.1589 91.2681 0001121 93.2185 266.8946 15.34406134 05
| Epoch (UTC): | 25 May 2026 12:58:57 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 91.2681° |
| argument of perigee: | 93.2185° |
| revolutions per day: | 15.34406134 |
| mean anomaly at epoch: | 266.8946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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