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 64768U 26145.64104236 +.00000000 +00000-0 +53199-3 0 00008
2 64768 53.1597 235.3581 0000938 107.2991 252.8113 15.30210583 09
| Epoch (UTC): | 25 May 2026 15:23:06 |
| Eccentricity: | 0.0000938 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3581° |
| argument of perigee: | 107.2991° |
| revolutions per day: | 15.30210583 |
| mean anomaly at epoch: | 252.8113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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