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 41339U 26099.17547777 +.00000000 +00000-0 +23588-3 0 00003
2 41339 31.0051 62.0052 0008685 84.0651 276.0979 15.17995788 08
| Epoch (UTC): | 09 April 2026 04:12:41 |
| Eccentricity: | 0.0008685 |
| inclination: | 31.0051° |
| perigee height: | 506 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 62.0052° |
| argument of perigee: | 84.0651° |
| revolutions per day: | 15.17995788 |
| mean anomaly at epoch: | 276.0979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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