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 64549U 26145.26507635 +.00000000 +00000-0 +28348-3 0 00001
2 64549 97.4758 261.5331 0002159 139.3753 220.7645 15.23529109 02
| Epoch (UTC): | 25 May 2026 06:21:42 |
| Eccentricity: | 0.0002159 |
| inclination: | 97.4758° |
| perigee height: | 494 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 261.5331° |
| argument of perigee: | 139.3753° |
| revolutions per day: | 15.23529109 |
| mean anomaly at epoch: | 220.7645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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