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 64389U 26145.59709132 +.00000000 +00000-0 +48534-3 0 00004
2 64389 43.0007 105.9198 0000794 211.1920 148.8884 15.27580228 06
| Epoch (UTC): | 25 May 2026 14:19:48 |
| Eccentricity: | 0.0000794 |
| inclination: | 43.0007° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 105.9198° |
| argument of perigee: | 211.1920° |
| revolutions per day: | 15.27580228 |
| mean anomaly at epoch: | 148.8884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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