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 65681U 26145.30523182 +.00000000 +00000-0 +72820-3 0 00003
2 65681 53.1608 349.8085 0001064 98.7738 261.3383 15.30201834 04
| Epoch (UTC): | 25 May 2026 07:19:32 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.8085° |
| argument of perigee: | 98.7738° |
| revolutions per day: | 15.30201834 |
| mean anomaly at epoch: | 261.3383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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