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 26145.43191155 +.00000000 +00000-0 +66985-4 0 00000
2 39091 98.3990 325.4317 0009234 313.0698 46.9715 14.36531641 01
| Epoch (UTC): | 25 May 2026 10:21:57 |
| Eccentricity: | 0.0009234 |
| inclination: | 98.3990° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 325.4317° |
| argument of perigee: | 313.0698° |
| revolutions per day: | 14.36531641 |
| mean anomaly at epoch: | 46.9715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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