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 39446U 26145.42164723 +.00000000 +00000-0 +42318-3 0 00007
2 39446 97.8683 101.3475 0050292 37.5590 322.9127 14.96798686 07
| Epoch (UTC): | 25 May 2026 10:07:10 |
| Eccentricity: | 0.0050292 |
| inclination: | 97.8683° |
| perigee height: | 542 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 101.3475° |
| argument of perigee: | 37.5590° |
| revolutions per day: | 14.96798686 |
| mean anomaly at epoch: | 322.9127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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