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 39172U 26076.91211037 +.00000000 +00000-0 +00000-0 0 00000
2 39172 0.0592 288.5480 0001734 88.4442 86.3324 1.00271133 04
| Epoch (UTC): | 17 March 2026 21:53:26 |
| Eccentricity: | 0.0001734 |
| inclination: | 0.0592° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 288.5480° |
| argument of perigee: | 88.4442° |
| revolutions per day: | 1.00271133 |
| mean anomaly at epoch: | 86.3324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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