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 39766U 26159.54979360 +.00000000 +00000-0 +20114-3 0 00001
2 39766 97.9210 256.8376 0001672 90.6305 269.5098 14.79472067 03
| Epoch (UTC): | 08 June 2026 13:11:42 |
| Eccentricity: | 0.0001672 |
| inclination: | 97.9210° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 256.8376° |
| argument of perigee: | 90.6305° |
| revolutions per day: | 14.79472067 |
| mean anomaly at epoch: | 269.5098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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