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 64564U 26145.56472948 +.00000000 +00000-0 +24297-3 0 00008
2 64564 97.7683 260.2413 0002013 30.5297 329.6040 14.94776882 07
| Epoch (UTC): | 25 May 2026 13:33:12 |
| Eccentricity: | 0.0002013 |
| inclination: | 97.7683° |
| perigee height: | 582 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 260.2413° |
| argument of perigee: | 30.5297° |
| revolutions per day: | 14.94776882 |
| mean anomaly at epoch: | 329.6040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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