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 64272U 26145.25249383 +.00000000 +00000-0 +44507-3 0 00001
2 64272 53.1605 121.3911 0001217 132.2948 227.8156 15.30210898 09
| Epoch (UTC): | 25 May 2026 06:03:35 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.3911° |
| argument of perigee: | 132.2948° |
| revolutions per day: | 15.30210898 |
| mean anomaly at epoch: | 227.8156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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