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 64276U 26145.33702014 +.00000000 +00000-0 +80645-3 0 00002
2 64276 53.1595 118.3682 0001414 88.1594 271.9571 15.35408403 04
| Epoch (UTC): | 25 May 2026 08:05:18 |
| Eccentricity: | 0.0001414 |
| inclination: | 53.1595° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 118.3682° |
| argument of perigee: | 88.1594° |
| revolutions per day: | 15.35408403 |
| mean anomaly at epoch: | 271.9571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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