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 64437U 26145.55230742 +.00000000 +00000-0 +81686-3 0 00005
2 64437 70.0007 240.5294 0003391 272.3463 87.7308 14.98339294 04
| Epoch (UTC): | 25 May 2026 13:15:19 |
| Eccentricity: | 0.0003391 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5294° |
| argument of perigee: | 272.3463° |
| revolutions per day: | 14.98339294 |
| mean anomaly at epoch: | 87.7308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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