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 64275U 26145.24932889 +.00000000 +00000-0 +45191-3 0 00003
2 64275 53.1598 121.3681 0001191 116.1049 244.0075 15.30210584 04
| Epoch (UTC): | 25 May 2026 05:59:02 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.3681° |
| argument of perigee: | 116.1049° |
| revolutions per day: | 15.30210584 |
| mean anomaly at epoch: | 244.0075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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