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 65211U 26145.32623550 +.00000000 +00000-0 +62968-3 0 00006
2 65211 53.1572 156.7734 0000907 74.9679 285.1422 15.30212936 07
| Epoch (UTC): | 25 May 2026 07:49:46 |
| Eccentricity: | 0.0000907 |
| inclination: | 53.1572° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 156.7734° |
| argument of perigee: | 74.9679° |
| revolutions per day: | 15.30212936 |
| mean anomaly at epoch: | 285.1422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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