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 64515U 26145.37791919 +.00000000 +00000-0 +30299-3 0 00004
2 64515 51.9000 191.5585 0001524 73.9486 286.1644 14.79888136 07
| Epoch (UTC): | 25 May 2026 09:04:12 |
| Eccentricity: | 0.0001524 |
| inclination: | 51.9000° |
| perigee height: | 629 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 191.5585° |
| argument of perigee: | 73.9486° |
| revolutions per day: | 14.79888136 |
| mean anomaly at epoch: | 286.1644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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