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 39741U 26145.52529390 +.00000000 +00000-0 +00000-0 0 00000
2 39741 56.5091 332.3994 0038419 326.8930 32.8791 2.00562712 06
| Epoch (UTC): | 25 May 2026 12:36:25 |
| Eccentricity: | 0.0038419 |
| inclination: | 56.5091° |
| perigee height: | 20080 km |
| apogee height: | 20284 km |
| right ascension of ascending node: | 332.3994° |
| argument of perigee: | 326.8930° |
| revolutions per day: | 2.00562712 |
| mean anomaly at epoch: | 32.8791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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