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 64308U 26145.31169108 +.00000000 +00000-0 +13961-3 0 00004
2 64308 70.0015 1.3478 0002638 270.6108 89.4749 14.98335282 08
| Epoch (UTC): | 25 May 2026 07:28:50 |
| Eccentricity: | 0.0002638 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3478° |
| argument of perigee: | 270.6108° |
| revolutions per day: | 14.98335282 |
| mean anomaly at epoch: | 89.4749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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