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 65464U 26145.30983789 +.00000000 +00000-0 +46405-3 0 00005
2 65464 53.1590 261.6471 0000928 96.7196 263.3911 15.31714819 09
| Epoch (UTC): | 25 May 2026 07:26:09 |
| Eccentricity: | 0.0000928 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 261.6471° |
| argument of perigee: | 96.7196° |
| revolutions per day: | 15.31714819 |
| mean anomaly at epoch: | 263.3911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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