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 64513U 26145.57459966 +.00000000 +00000-0 +26341-3 0 00000
2 64513 51.9002 242.5969 0001831 118.6904 241.4243 14.81660732 05
| Epoch (UTC): | 25 May 2026 13:47:25 |
| Eccentricity: | 0.0001831 |
| inclination: | 51.9002° |
| perigee height: | 623 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 242.5969° |
| argument of perigee: | 118.6904° |
| revolutions per day: | 14.81660732 |
| mean anomaly at epoch: | 241.4243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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