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 64265U 26145.32097691 +.00000000 +00000-0 +37609-3 0 00009
2 64265 53.1614 121.1065 0001141 88.2917 271.8214 15.30204987 07
| Epoch (UTC): | 25 May 2026 07:42:12 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.1065° |
| argument of perigee: | 88.2917° |
| revolutions per day: | 15.30204987 |
| mean anomaly at epoch: | 271.8214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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