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 65227U 26145.13914361 +.00000000 +00000-0 +55299-3 0 00004
2 65227 97.6708 210.3400 0004321 2.8216 357.3029 14.97566527 01
| Epoch (UTC): | 25 May 2026 03:20:22 |
| Eccentricity: | 0.0004321 |
| inclination: | 97.6708° |
| perigee height: | 571 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 210.3400° |
| argument of perigee: | 2.8216° |
| revolutions per day: | 14.97566527 |
| mean anomaly at epoch: | 357.3029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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