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 64089U 26145.62932572 +.00000000 +00000-0 +28212-3 0 00002
2 64089 97.4690 220.2165 0010957 112.9740 247.2648 15.13013293 09
| Epoch (UTC): | 25 May 2026 15:06:13 |
| Eccentricity: | 0.0010957 |
| inclination: | 97.4690° |
| perigee height: | 519 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 220.2165° |
| argument of perigee: | 112.9740° |
| revolutions per day: | 15.13013293 |
| mean anomaly at epoch: | 247.2648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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