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 64519U 26145.56022968 +.00000000 +00000-0 +28505-3 0 00007
2 64519 51.8997 240.6628 0000989 89.5836 270.5239 14.79949908 07
| Epoch (UTC): | 25 May 2026 13:26:43 |
| Eccentricity: | 0.0000989 |
| inclination: | 51.8997° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 240.6628° |
| argument of perigee: | 89.5836° |
| revolutions per day: | 14.79949908 |
| mean anomaly at epoch: | 270.5239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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