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 39168U 26144.86035779 +.00000000 +00000-0 +00000-0 0 00002
2 39168 0.0187 291.6352 0000397 51.9161 156.1185 1.00271056 04
| Epoch (UTC): | 24 May 2026 20:38:54 |
| Eccentricity: | 0.0000397 |
| inclination: | 0.0187° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 291.6352° |
| argument of perigee: | 51.9161° |
| revolutions per day: | 1.00271056 |
| mean anomaly at epoch: | 156.1185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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