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 64525U 26145.33610958 +.00000000 +00000-0 +76578-4 0 00005
2 64525 51.9037 261.7779 0000542 118.4342 241.6676 14.79932466 05
| Epoch (UTC): | 25 May 2026 08:03:59 |
| Eccentricity: | 0.0000542 |
| inclination: | 51.9037° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 261.7779° |
| argument of perigee: | 118.4342° |
| revolutions per day: | 14.79932466 |
| mean anomaly at epoch: | 241.6676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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