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 39574U 26145.61994388 +.00000000 +00000-0 +22313-3 0 00001
2 39574 64.9737 23.7653 0011871 266.1168 93.8616 15.45131628 09
| Epoch (UTC): | 25 May 2026 14:52:43 |
| Eccentricity: | 0.0011871 |
| inclination: | 64.9737° |
| perigee height: | 423 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 23.7653° |
| argument of perigee: | 266.1168° |
| revolutions per day: | 15.45131628 |
| mean anomaly at epoch: | 93.8616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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