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 39011U 26145.28908990 +.00000000 +00000-0 +49951-4 0 00002
2 39011 63.3550 348.9459 0433697 26.9630 335.3228 13.45514829 06
| Epoch (UTC): | 25 May 2026 06:56:17 |
| Eccentricity: | 0.0433697 |
| inclination: | 63.3550° |
| perigee height: | 765 km |
| apogee height: | 1413 km |
| right ascension of ascending node: | 348.9459° |
| argument of perigee: | 26.9630° |
| revolutions per day: | 13.45514829 |
| mean anomaly at epoch: | 335.3228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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