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 64316U 26145.02377919 +.00000000 +00000-0 -11993-3 0 00006
2 64316 70.0015 1.9454 0002523 268.6431 91.4439 14.98337411 01
| Epoch (UTC): | 25 May 2026 00:34:14 |
| Eccentricity: | 0.0002523 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.9454° |
| argument of perigee: | 268.6431° |
| revolutions per day: | 14.98337411 |
| mean anomaly at epoch: | 91.4439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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