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 45397U 26145.32681383 +.00000000 +00000-0 +51086-3 0 00006
2 45397 53.0521 121.3481 0002729 51.2514 308.8740 15.55511591 02
| Epoch (UTC): | 25 May 2026 07:50:36 |
| Eccentricity: | 0.0002729 |
| inclination: | 53.0521° |
| perigee height: | 399 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 121.3481° |
| argument of perigee: | 51.2514° |
| revolutions per day: | 15.55511591 |
| mean anomaly at epoch: | 308.8740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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