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 39767U 26145.53519771 +.00000000 +00000-0 +18651-3 0 00005
2 39767 97.8039 243.0036 0005619 38.9985 321.1640 14.95735628 08
| Epoch (UTC): | 25 May 2026 12:50:41 |
| Eccentricity: | 0.0005619 |
| inclination: | 97.8039° |
| perigee height: | 576 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 243.0036° |
| argument of perigee: | 38.9985° |
| revolutions per day: | 14.95735628 |
| mean anomaly at epoch: | 321.1640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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