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 65649U 26144.68094551 +.00000000 +00000-0 +44863-3 0 00006
2 65649 53.1588 314.2412 0000775 73.8874 286.2212 15.30204285 08
| Epoch (UTC): | 24 May 2026 16:20:33 |
| Eccentricity: | 0.0000775 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.2412° |
| argument of perigee: | 73.8874° |
| revolutions per day: | 15.30204285 |
| mean anomaly at epoch: | 286.2212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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