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 64295U 26145.32822434 +.00000000 +00000-0 +13226-3 0 00002
2 64295 70.0024 1.4002 0002743 269.7865 90.2980 14.98334149 01
| Epoch (UTC): | 25 May 2026 07:52:38 |
| Eccentricity: | 0.0002743 |
| inclination: | 70.0024° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.4002° |
| argument of perigee: | 269.7865° |
| revolutions per day: | 14.98334149 |
| mean anomaly at epoch: | 90.2980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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