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 39643U 26154.32139433 +.00000000 +00000-0 +16394-3 0 00000
2 39643 65.0111 41.7227 0017625 280.7998 79.1104 14.34716714 08
| Epoch (UTC): | 03 June 2026 07:42:48 |
| Eccentricity: | 0.0017625 |
| inclination: | 65.0111° |
| perigee height: | 763 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 41.7227° |
| argument of perigee: | 280.7998° |
| revolutions per day: | 14.34716714 |
| mean anomaly at epoch: | 79.1104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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