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 39091U 26155.74043161 +.00000000 +00000-0 +84090-4 0 00005
2 39091 98.3992 335.4846 0008969 278.5862 81.4309 14.36537037 01
| Epoch (UTC): | 04 June 2026 17:46:13 |
| Eccentricity: | 0.0008969 |
| inclination: | 98.3992° |
| perigee height: | 764 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 335.4846° |
| argument of perigee: | 278.5862° |
| revolutions per day: | 14.36537037 |
| mean anomaly at epoch: | 81.4309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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