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 64445U 26145.26552965 +.00000000 +00000-0 +34242-3 0 00002
2 64445 53.1585 93.1014 0001958 85.8921 274.2303 15.30203642 03
| Epoch (UTC): | 25 May 2026 06:22:21 |
| Eccentricity: | 0.0001958 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 93.1014° |
| argument of perigee: | 85.8921° |
| revolutions per day: | 15.30203642 |
| mean anomaly at epoch: | 274.2303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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