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 64271U 26145.62116858 +.00000000 +00000-0 +47592-3 0 00008
2 64271 53.1567 119.4287 0001287 88.1123 272.0025 15.30210935 09
| Epoch (UTC): | 25 May 2026 14:54:28 |
| Eccentricity: | 0.0001287 |
| inclination: | 53.1567° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.4287° |
| argument of perigee: | 88.1123° |
| revolutions per day: | 15.30210935 |
| mean anomaly at epoch: | 272.0025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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