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 64416U 26145.54794985 +.00000000 +00000-0 +28969-3 0 00000
2 64416 70.0006 240.5214 0003470 269.3527 90.7234 14.98339038 05
| Epoch (UTC): | 25 May 2026 13:09:02 |
| Eccentricity: | 0.0003470 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5214° |
| argument of perigee: | 269.3527° |
| revolutions per day: | 14.98339038 |
| mean anomaly at epoch: | 90.7234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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