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 64322U 26145.43481562 +.00000000 +00000-0 +16936-2 0 00008
2 64322 42.9989 286.6897 0001694 274.7633 85.3041 15.70946168 06
| Epoch (UTC): | 25 May 2026 10:26:08 |
| Eccentricity: | 0.0001694 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.6897° |
| argument of perigee: | 274.7633° |
| revolutions per day: | 15.70946168 |
| mean anomaly at epoch: | 85.3041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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